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st 

MISSION DEVELOPMENT SIMULATOR 

PHASE 0 

SYSTEM TEST PROCEDURE 

REV 0 

DATE 3/20/69 

EY 5161 

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INTERNAL SIGN-OFF SHEET 

R. N. Noll, Manager 

Software Applications 

R. Sody,Nuality Specialist 

Mechanical Quality Engineering 

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TABLE OF CONTENTS 

1.0 SCOPE 

2.0 APPLICABLE DOCUMENTS 

3.0 SYSTEM VERIFICATION AND DEMONSTRATION TESTS 

3.1 VALIDATION OF DATA 

4.0 VERIFICATION TEST PROCEDURES 

5.0 DEMONSTRATION TEST PROCEDURES 

5.1 PRE-TEST CHECKOUT PROGRAM 

5.2 ATS ONLY DOP 

5.3 MO ONLY DOP 

5.4 ATS /M0 DOP 

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1.0 SCOPE 

This Document is the Test Procedure for demonstration and verification 

of the Phase 0 capability of the MDS. 

2.0 APPLICABLE DOCUMENTS 

1) Mission Development Simulator Performance Design Requirements. 

SAFSL Exhibit 34003, 15 August 1968 

2) Phase 0 Configuration Presentation 

Made 6/26/68, BIN-50372-96-3 

3) Phase 0 - Simulation Software Requirement Rev 2 

October 15, 1968 BIN: BIF-055-1318-20-3-68 

4) Mission Development Simulator Phase 0 Demonstration Requirements. 

BIF-055-50372-244-268 

5) Mission Development Simulator Phase 0 System Test Plan Rev C 

1/30/69 

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3.0 SYSTEM VERIFICATION AND DEMONSTRATION 

The overall function characteristics of the Phase 0 will be verified and demonstrated during a series of System Level Tests, 

Anaylsis of Subsystem Data and Visual Inspection of the Hardware. 

The Procedures in this Document are categorized as follows: 

1) Verification Tests (Section 4.0. These Tests will be performed 

during Hardware/Software Integration Tests). 

a) Visual Inspection of Hardware and/or Design Drawings 

b) Individual measurements made at the System Level but not 

included in the Script of the DOP'S. 

c) Analysis of Subsystem and System Test Data 

d) Pre-Test Checkout Program and Procedure 

e) Demonstration Orbital Passes 

2) Demonstration Tests (Section 5.0. These Tests will be performed 

during the Demonstration Test Period) 

a) Pre-Test Checkout 

b) Demonstration Orbital Passes 

c) Review of Analytical Data 

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3.1 Validation of Data 

All Data taken for verification of Requirements shall be identified, dated and initialed by the Test Conductor, Quality Assurance, 

AFQA and AFSO to validate that the Test Procedure was followed. 

3.1.1 Deviations from Procedure 

Any Deviations from the Test Procedure will be noted 

in the Test Log Book and in the margin of the Procedure 

and initialed by the Test Conductor, Quality Assurance, 

AFQA and AFSO. Data taken during Tests where there are 

deviations from the Procedures will not be submitted for 

verification until the deviation is approved by the AFSO. 

3.1.2 Classification of Deviations from Procedures 

3.1.2.1 For the purpose of this Document, Deviations 

shall be considered only 

1) Difference in the location from which Data 

is recorded. Most Data will be recorded 

via Patchcords from the System Junction Box. 

2) Difference in the type of Signals recorded. 

3) Difference in the method of Interpreting recorded Data. 

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3.1.3 Reverification of Requirements 

In the event of a Hardware and/or Software change that 

could affect Data previously taken, the Test Conductor 

shall note the change and Test affected in the Test Log 

Book. These Tests will be re-run to verify the affected 

Data. 

3.1.4 Test Software 

Test Software is required for Tests specified in 4.28 and 

4.29. 

3.1.4.1 Special Program No. 1- This Program is designed 

to command the HPA and LPA Elevators and transport and Elevators in Sequence to verify the 1.0 

second slide change requirement on the Hardware. 

3.1.4.2 Special Program No. 2 - This Program is designed 

to command the HPA and LPA Elevators and transports to skip 5 slides and load the sixth into 

the viewing station within 3.0 seconds. 

4.0 Verification of Requirements 

This Section is the Procedures to be used for verification of requirements 

and the Tests specified will be completed during the Hardware/Software 

Integration Test Period. 

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4.0 Continued 

Each major paragraph, Ex 4.1, 4.2 etc., is a complete Procedure 

and is not dependent upon any other major paragraph or Procedure. 

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4.1 Requirement Title: PERFORMANCE DEMONSTRATIONS 

4.1.1 Requirement Paragraph in the Test Requirements Document 

3.0 (a) 

4.1.2 Requirement 

The overall functional characteristics of the Phase 0 

MDS, its operability characteristics, and certain of 

the specific performance and hardware/software design 

requirements will be demonstrated. General capabilities 

to be demonstrated are: 

a) Pre-test checkout program and procedure. 

4.1.3 Related Paragraph in System Test Plan 

4.1 

4.1.4 Verification Test Procedure 

The Test Procedure is defined in Test Plan/Procedure for 

The Pre-Test Checkout Program. BIN: BIF-055-46753-69. 

Dated 

The Procedure has been separated from this Procedure 

since it will also be used as a Daily Procedure during 

Operations to check simulator Hardware by use of 

appropriate Software. 

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4.2 Requirement Title: PERFORMANCE DEMONSTRATION 

4.2.1 Requirement Paragraph Test Requirements Document 

3.0 (b) 

4.2.2 Requirement 

All controls and displays on Panels 2C, 2D, 3B and 7B 

of the SLM. 

4.2.3 Related Paragraph System Test Plan 

4.2 

4.2.4 Pre-Test Requirements 

None 

4.2.5 Verification Test Procedure 

No Test required. Requirement will be demonstrated 

during DOP's. 

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4.3 Requirement Title: PERFORMANCE DEMONSTRATION 

4.3.1 Requirement Paragraph Test Requirements Document 

3.0 (c) 

4.3.2 Requirement 

All controls and displays on Panels IA, 1B, 2A, 2B 

5A and 5B of the SCC. 

4.3.3 Related Paragraph in System Test Plan 

4.3 

4.3.4 Pre-Test Requirements: 

None 

4.3.5 Verification Test Procedure 

No Test required. Requirement is verified by 4.1 

Attach Copy of 4.1 Procedure to these data sheets. 

No Test required. All controls and displays are verified 

during 4.1. Attach a copy of the data sheets from 4.1 

to this data sheet. 

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4.4 Requirement Title: PERFORMANCE DEMONSTRATION 

4.4.1 Requirement Paragraph in Test Requirements Document 

3.0 (e) 

4.4.2 Requirement 

The single ATS mode and the single MO Mode (peripheral 

display at 60°) 

4.4.3 Related Paragraph in System Test Plan 

4.4 

4.4.4 Pre-Test Requirements: 

None 

4.4.5 Verification Test Procedure 

No Test required. Requirement Will be demonstrated during 

ATS/MO DOP's 

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4.5 Requirement Title: PERFORMANCE DEMONSTRATION 

4.5.1 Requirement Paragraph in Test Requirements Document 

3.0 

4.5.2 Requirement 

Test and operations, data collection and reduction 

capability. 

4.5.3 Related Paragraph in System Test Plan 

4.5 

4.5.4 Pre-Test Requirements 

4.5.4.1 Test Team 

Test Conductor 

Technicians 

Quality Assurance Init 

AFQA Init 

Aerospace Observer Init 

AFSO Init 

4.5.4.2 Test Equipment Required 

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4.5.4.3 Equipment Confidence Status 

The Test Conductor will insure that all Test 

Equipment has a valid calibration sticker. 

Equipment Type Cal Date 

4.5.4.4 Subsystems Status 

The following are required to be active during 

this Test. 

ON OFF 

SCC X 

SLM X 

DIU X 

Stimulus S/S X 

Computer S/S X 

4.5.4.5 Power Turn On 

Turn Power on to all Subsystems 

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4.5.5 Verification Test Procedure 

4.5.5.1 Load an ATS Only DOP into the SDS 930 Computer. 

4.5.5.2 Select ten (10) functions to be recorded on 

strip chart recorders and the performance data 

collection tape. 

Functions 

1) Magnification Control Stick Setting in ATS Range 

2) HPA/LPA Select 

3) HPA Blanking Command 

4) LPA Blanking Command 

5) RSS Stick Deflection 

6) End Stop Signal 

LPA X Position Value (On Analog Twice. Low 

7) Scale and High Scale) 

LPA Y Position Value (On Analog Twice. Low 

8) Scale and High Scale) 

9) LPA X Coordinate Rate .(Twice on Analog 

10) HPA Y Coordinate Rate (Twice on Analog) 

11) MO Measured Pitch Angle 

4.5.5.3 Set the recorder chart speed at 20 mm/sec and 

turn On the recorders. 

4.5.5.4 Activate the resume switch to start and complete 

the DOP run. 

4.5.5.5 After completion of the DOP, process the Performance data collection tape to provide a printed 

stripped and merged data list. 

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4.5.5.6 Compare the printed list to the strip chart 

recordings and verify that the same functions 

have been collected and reduced. 

Verified 

4.5.5.7 Attach all data to these data sheets for review to verify the consistency and accuracy 

of the reduced data. 

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4.6 Requirement Title: PERFORMANCE DEMONSTRATION 

4.6.1 Requirement Paragraph in Test Requirements Document 

1) 3.0 (i) 

2) 3.3.2.1.2 

4.6.2 Requirement 

1) Turn around capability (10 & 30 minutes) 

2) AN Automatic Restacking capability is provided 

4.6.3 Related Paragraph in System Test Plan 

4.6 

4.6.4 Pre-Test Requirements 

4.6.4.1 Test Team 

Test Conductor 

Technicians 

Quality Assurance Init 

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4.6.4.1 Continued 

AFQA Init 

Aerospace Observer Init 

APS() Init 

4.6.4.2 Test Equipment Required 

1) Stopwatch 

4.6.4.3 Equipment Confidence Status 

The Test Conductor will insure that all Test 

Equipment has a valid calibration Sticker. 

Equipment Type Cal Date 

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4.6.4.4 Subsystems Status 

The following are required to be active during this Test. 

ON OFF 

SCC X 

SLM X 

DIU X 

Stimulus S/S X 

Computer S/S X 

4.6.4.5 Power Turn On 

This Test will be performed at the conclusion 

of the ATS only DOP. Power will already be 

applied to all Subsystems. 

4.6.5 Verification Test Procedure 

4.6.5.1 The Script contains a restack Flag at 

the conclusion of one of the DOP'S. Depress 

the Special Interrupt switch at the SCC and 

at the same time start the Stopwatch. 

4.6.5.2 The following tasks shall be completed: 

1) Automatic restacking by the computer. 

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4.6.5.2 Continued 

1) Continued - The completion of restacking will be indicated on the CRT 

display which will indicate that all 

slides have been returned to their 

original order. 

2) Manual restacking of the cues. The cue 

projector shall be returned to position 

1 manually or by use of the remote control 

unit. 

3) All switches at the SLM shall be reset 

to the positions indicated in the DOP 

procedure. 

4.6.5.3 When the CRT display indicates that restacking 

is completed, stop the stopwatch, stop all 

activity on items 2 and 3 and remove the supply and takeup elevators from each leg of the 

SVS. Verify that all slides were returned to 

the original order according to the script. 

Verified 

4.6.5.4 Return all magazines and reload the DOP into 

the computer. 

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4.6.5.5 Stop the Stopwatch and activate the resume 

switch. The program shall be allowed to 

complete the first target group. 

4.6.5.6 Record the elapsed time on the Stopwatch. 

Min. Req is 10 minutes or less 

4.6.5.7 At the conslusion of the DOP, start the 

Stopwatch and verify that the following 

tasks are completed. 

1) Remove all magazines from both legs 

of the SVS and replace with different 

magazines. 

2) Remove the cue casset and replace 

with a different casset. 

3) Reload the computer program to run a 

different DOP. 

4.6.5.8 When the above items have been completed, 

activate the resume switch and stop the 

Stopwatch. The program shall complete the DOP. 

4.6.5.9 Record the elapsed time on the Stopwatch. 

Min. Req is 30 minutes or less. 

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4.7 Requirement Title: PERFORMANCE DEMONSTRATION 

4.7.1 Requirement Paragraph Test Requirements Document 

3.0 (j) 

4.7.2 Requirement 

Operational Scripting capability. 

4.7.3 Related Paragraph in System Test Plan 

4.7 

4.7.4 Pre-Test Requirements 

None 

4.7.5 Verification Test Procedure 

No Test Required. Requirement will be demonstrated by 

Running DOP's. 

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4.8 Requirement Title: PRIMARY PERFORMANCE CHARACTERISTICS 

4.8.1 Requirement Paragraph in Test Requirements Document 

1) 3.1.1.1 

2) 3.3.3 

4.8.2 Requirement 

1) Validate the adherence of the MDS to a mutually agreed 

AVE baseline established for Phase 0 on May 1, 1968, 

except the SLM Panels 2C and 2D which were established 

on June 30, 1968. The software for Phase 0 will be 

frozen to the Phase 0 Simulation Software Requirements 

Revision 2. 

2) Verify Panels 2C and 2D to insure that these two panels 

reflect the AVE configuration as presented on: 

Drawing 711-03063 2 July 1968 for Panel 2C 

Drawing 711-03064 2 July 1968 for Panel 2C 

Panels 3B and 7B will also be active. Panels 6C and 

3C contain simulation peculiar switches. All other 

panels of the SLM will be blank for Phase O. 

4.8.3 Related Paragrapn in System Test Plan 

4.8 

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4.8.4 Pre-Test Requirements 

None 

4.8.5 Verification Test Procedure 

4.8.5.1 Compare AVE Panel Configuration with Simulator 

Configuration by comparing AVE drawings with the 

actual panels. 

AVE Dwg. 

Panel 2C 711-03063 

Panel 2D 711-03064 

Verified 

4.8.5.2 The controls on Panels 3B, 7B 3C and 6C have 

been verified by 4.1 (Pre-checkout Program) 

4.8.5.3 Verify by inspection that all other Panels are 

Blank. 

Verified 

4.8.5.4 The calibrated test results from the individual 

CPC Tests for Drive Control Response and Position 

Simulation shall be available for Review. 

4.8.5.5 Demonstration Test Procedure 

None 

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4.9 Requirement Title: TIMING SUBSYSTEM 

4.9.1 Requirement Paragraph in Test Requirements Document 

3.1.1.1.3.2 

4.9.2 Requirement 

One event timer shall be driven. 

4.9.3 Related Paragraph in System Test Plan 

4.9 

4.9.4 Pre-Test Requirements: 

None 

4.9.5 Verification Test Procedure 

No Test required. Requirement will be demonstrated during 

DOP's. 

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4.10 Requirement Title: IMAGE VELOCITY SENSOR 

4.10.1 Requirement paragraph in test requirements 

document 

3.1.1.1.5.3 

4.10.2 Requirement 

IVS errors::to•be simulated are random errors. 

Saturation will be simulated in the event of 

clouds (when prescripted) in which case the 

saturate light will be turned on and the IVS 

output will limit. Normal IVS rate - nulling 

will be simulated in the range of 540u rad/sec 

and when IVS is enabled the rate will be reduced 

to approximately 

4.10.3 Related paragraph in system test Plan 

4.10 

4.10.4 Pre-test Requirements 

None 

4.10.5 Verification Test Procedure 

No test required. The test results from the 

individual CPC tests verifying this requirement 

shall be attached to these data sheets. 

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4.11 Requirement Title: STICK INPUT 

4.11.1 Requirement Paragraph in Test Requirements 

Document 

3.1.1.1.5.4 

4.11.2 Requirement: 

The stick polarity shall be reversable between 

runs. The stick shall allow low rates to be 

inserted into the device system. The transfer 

function shall be provided by the Drive Connection 

Module of the On-Board Software. 

4.11.3 Related Paragraph in System Test Plan 

4.11 

4.11.4 Pre-test Requirements 

None 

4.11.5 Verification Test Procedure 

No test required. The test results from the 

individual CPC tests verifying this requirement 

shall be attached to these data sheets. Requirement 

will also be demonstrated during DOP. 

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4.12 Requirement Title: MAGNIFICATION AND REAL FIELD OF VIEW 

4.12.1 Requirement Paragraph in Test Requirement Document 

3.1.1.1.7.1.1 

4.12.2 Requirement 

Demonstrate that the MDS shall follow operator commands 

and reach any commanded value within 0.5 second and that 

the step from 31.76X + 5% to 63.5X + 5% shall occur in 

1.0 second or less. (See paragraph 3.1.1.1.7.1.5) for 

a discussion of presentation rates). Verify that the 

simulated real field-of-view is 3.78 degrees at 15.88X, 

and 0.945 degree at 63.5X with the field varying inversely with zoom to the higher powers in each range. 

4.12.3 Related Paragraph in System Test Plan 

4.12 

4.12.4 Pre-Test Requirements 

4.12.4.1 Test Team 

Test Conductor 

Technicians 

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4.12.4.1 Continued 

Quality Assurance Init 

AFQA Init 

Aerospace Observer Init 

AFSO Init 

4.12.4.2 Test Equipment Required 

1) Techniwrite Model TR6460 Event Recorder or 

equivalent. 

2) T-Boxes S/N 4605-and S/N 4605- 

3) Eng Test Box SK56179-999 

4) HP 3460B Digital Voltmeter or equivalent 

5) Brush Mark 200B Analog Recorder or equivalent 

6) Graduated Test Slide 

4.12.4.3 Equipment Confidence Status 

The Test Conductor will insure that all Test 

Equipment has a valid calibration sticker. 

Equipment Type Cal Date 

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4.12.4.3 Continued 

Equipment Type Cal Date 

4.12.4.4 Subsystems Status 

The following are required to be active during 

this Test. 

ON OFF 

SCC X 

SLM X 

DIU X 

Stimulus S/S X 

Computer S/S X 

4.12.4.5 Power Turn On 

4.12.4.5 Install T-Boxes (S/N 4605- and S/N 4605- 

at the SVS Interface Connectors J1 and J2. 

Turn Power On to all Subsystems. 

4.12.5 Verification Test Procedure 

4.12.5.1 Install and connect the Engineering Test Box, 

Per SK56179-999 

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4.12.5.2 Turn On the HPA Holder Changer, Light Source 

and Spherical Zoom. 

4.12.5.3 Activate the Selector to HPA and Unblank HPA at 

the Eng. Test Box. 

4.12.5.4 Insert the graduated Test Slide into the HPA 

Viewing Station and verify that the High Power 

Arm is installed, and that the SVS Reticle is in 

place. 

4.12.5.5 Set the following Drive Voltages at the Engineering 

Test Box. 

Voltage 

Spherical Zoom 

K - Rotator 

Iris Zoom 

Cyl Zoom 1 

Cyl Zoom 2 

Determined 

by 

Eng Analysis 

The X and Y Drives and Filter Modulator will be 

used to center the Slide and adjust the intensity 

to a comfortable Level. 

4.12.5.6 Center the Test Slide in the FOV using the X and Y 

Drive and measure the FOV. 

Inches 

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4.12.5.7 Change the Spherical Zoom Drive Voltage to 

V and measure the FOV. 

Inches 

4.12.5.8 Remove the High Power Aim and install the Low 

Power Arm. 

4.12.5.9 Change the Spherical Zoom Drive Voltage to V 

and measure the FOV. 

Inches 

4.12.5.10 Change the Spherical Zoom Drive Voltage to 

and measure the FOV. 

Inches 

4.12.5.11 Attach the Photometer Mount and Photometer to the 

Supplemental Eyepiece. 

4.12.5.12 Locate the center of the Photometer Spot on the 

left hand edge of the FOV, and record the angle 

from Normal. 

Degrees. 

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4.12.5.13 Locate the Spot on the right hand edge of the FOV 

and record the angle from Normal. Degrees 

The sum of the two Angles should be 60° + 

4.12.5.14 The above Data shall be used to perform the following 

Analysis: 

The objective here is to verify that the system will 

simulate the correct fields of view at the specified 

magnifications. In particular, this is a problem of 

showing that the zoom and anamorphs will be driven correctly together to accomplish this objective. Choosing 

two cases at opposite extremes (nadir and = 45.870) 

will exercise the optical system sufficiently and 

allow calculation of FOV as described below. 

This analysis assumes nadir stimulus material for the 

present time. 

The real field of view (in inches) on the test slide 

can be determined by the following equation: 

X = 72912 x h x tan (sk + 1 OR- tan (01, - 1 OR) 

SF 2 2 

where: 

X = real FOV (in inches) at slide 

SF = stimulus scale factor 

h = altitude in nm. 

= aspect angle 

OR = OA = 60 = real FOV (in degree9) 

M M 

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Page 31 

4.12.5.14 Continued 

OA = apparent FOV (in degrees) 

M = system magnification 

The worst case aspect angles occur etc( m4x= 45.87° 

and 61/4 min= 00. 

Maximum and minimum X's can be determined for LPA 

and HPA yielding a total of four test points to be 

verified. 

For LPA, maximum X occurs when: h = 85 nm, 

SF = 128000:1, M = 15.88X, OR= 3.78°, oe = 45.87°. 

Minimum X occurs when: h = 75 nm, SK = 364000:1, 

M = 31.76X, OR = 1.89°, 04 = 0°. 

For HPA, maximum X occurs when: h = 85 nm, 

SF = 3200:1, M = 63.5X, OR = 0.945°, 04 = 45.87°. 

Minimum X occurs when: h = 75 nm, SF = 91000:1, 

M = 127X, OR = 0.472°, C4 = 0°. 

The values of X in both cases are 6.78 in. and 

.56 in. 

In order to set up the previous four test conditions, 

it is necessary to calculate the correct anamorph 

lens angles for maximum and minimum aspect angles. 

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4.12.5.14 Continued 

The following equations are used: 

sin = 2 ( 1 Vcos ok ) 

3RC 1 ITs774 

tan (II = sin 0 cos .0 

1 + sin2 6417677D sin2 

E -45° - + 

E2 = -450 ► +&/2 + F + 

Where Ek is the angle of the 1/2 power anamorph 

and E2 is the angle of the 2 power anamorph. For of. = 

45.87°, E1/2 = -1160 and E2 = -131° For 01( = 0°, 

Ek = E2 = 45°. 

For the zoom lens magnification, the following 

equation is used: 

3/2 

(Cosc4 sim Mo = h2stim 

cos 04 stim 

MN h2sim 

Where Mo = Zoom magnification at o( 

MN = Zoom magnification at nadir 

Assuming MN = .20X and nadir stimulus, the worst 

case zoom magnifications are .09X and .514X, This 

includes an additional 2:1 range needed after calculating worst case ranges with the above equation. 

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4.12.5.15 Remove the graduated Test Slide, Eng Test Box 

and leads that selected and unblanked HPA. 

4.12.5.16 Set up two Switches at the Beckman 2200 to Supply 

Step Commands from V to V for HPA 

and from V to V for LPA. The HPA 

Switch shall provide the step on T132 (Signal) 

and T133 (Return). The LPA shall provide the 

step on T120 (Signal) and T121 (Return). 

4.12.5.17 At the A2 Power Conditioning (SVS interface Connectors Jl and J2) install leads to record the 

following Signals. 

HPA SPH Zoom DR 

HPA SPH Zoom FB 

LPA SPH Zoom DR 

LPA SPH Zoom FB 

Channel Conn 

Jl - f, g 

J1 - BB, CC 

J2 - f, g 

J2 - BB, CC 

4.12.5.18 Set the Analog Recorder chart speed at 20 mm/Sec 

and turn On the recorders. 

4.12.5.19 Apply Step Voltages at the Beckman 2200. Record 

the elapsed time from initiation of Command to 

Settling of Feedback Signal to within +5%, as 

indicated by the change in Polarity of the Feedback Voltage. 

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4.12.5.19 Continued 

HPA LPA 

Sec Sec 

Time requirement for all Steps is 0.5 sec or less. 

Remove recordings and attach to these Data Sheets. 

4.12.5.20 Load an ATS Only DOP into the SDS 930 and verify 

that patchcords are installed at the system junction 

Step 

box to record the following: 

Supply Elevator Lower 

Supply Elevator Busy 

Transport Load 

Transport Busy 

Blanking Cmd 

Blanking FB 

HPA/LPA Select 

Reject 

HPA LPA 

28 3 

27 4 

34 12 

35 13 

37 15 

38 16 

1 X 

50 Y 

4.12.5.21 Verify that the targets are loaded in the HPA and 

LPA legs as follows: 

Supply Elev. Target # 

Position 1 1 Low Power 

2 2 Low Power 

Group 1 

3 3 Low Power 

4 4 High Power 

Group 2 

5 Empty 

Position 6 Empty 

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4.12.5.21 Continued 

Supply Elev. 

Position 7 

8 

9 

10 

11 

12 

13 

14 

15 

16 

Target # 

5 

6 

Empty 

Empty 

Empty 

Low Power 

Empty 

Empty 

Empty 

Empty 

Empty 

High Power 

4.12.5.22 Set chart speed on the event recorders at 20 MM/Sec 

and turn On the recorders. 

4.12.5.23 Activate the resume switch. When Slide #1 is in 

view, activate the reject switch. (Switch from 

target 1 to target 2) 

4.12.5.24 When target 2 is in view, activate the reject switch, 

(Switch from target 2 to target 3) 

4.12.5.25 When target 3 is in view, change magnification from 

31.76X to 63.5X (Change from LPA to HPA.) 

4.12.5.26 When target 4 is in view, change magnification from 

63.5X to 31.76X. (Change from HPA to LPA). Tlie script 

will lower the elevator one position so that to complete 

the elevator must raise and transport. 

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4.12.5.27 When target 3 is in view, activate the reject 

switch. (Skip 5 positions and view sixth) 

4.12.5.28 When target 5 is in view, change magnification from 

31.76X to 63.5X (Skip 5 positions and view sixth) 

4.12.5.29 When target 6 is in view, change magnification from 

63.5X to 31.76X (Skip 5 positions and view sixth) 

4.12.5.30 Activate freeze. Identify the slide change times 

on recorder paper. Remove recordings and attach to 

these data sheets. 

1) Target 1 to target 2 Secs 

2) Target 2 to target 3 Secs 

3) Target 3 to target 4 Secs 

4) Target 4 to target 3 Secs 

The requirement for the above changes is 1.0 

sec or less. For changes 1 and 2 the elapsed 

time is from the initiation of the reject 

command to shutter inblank. For changes 3 

and 4 the elapsed time is from initiation of 

magnification change to shutter unblank. 

5) Target 3 to target 5 Sec 

6) Target 5 to target 6 Sec 

7) Target 6 to target 5 Sec 

The requirement for the above changes is 3.0 

sec or less. The elapsed time is from initiation 

of the reject command to shutter unblank. 

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4.12.5.31 Repeat paragraphs 4.12.5.23 

the LPA Leg. 

to 4.12.5.30 for 

1) Target 1 to target 2 Sec 

2) Target 2 to target 3 Sec 

3) Target 3 to target 4 Sec 

4) Target 4 to target 3 Sec 

5) Target 3 to target 5 Sec 

6) Target 5 to target 6 Sec 

7) Target 6 to target 5 Sec 

4.12.5.32 Change magnification at various rates from 15.88X to 

31.76X, 31.76X to 15.88X. Remove the recordings 

for Zoom Drive and Feedback and verify that the 

BPA & LPA Zoom Servos follow Operator Commands. 

Attach the recordings to these Data Sheets. 

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4.13 Requirement Title: OTHER CHARACTERISTICS 

4.13.1 Requirement Paragraph in Test Requirement Document 

3.1.1.1.7.1.2.3 

4.13.2 Requirement 

Demonstrate that the headrest is of the same configuration 

as the June 30, 1968 AVE baseline with dimensional changes 

to adapt it for use with the supplemental eyepiece. 

4.13.3 Related Paragraph in System Test Plan 

4.13 

4.13.4 Pre-Test Requirements 

4.13.4.1 Test Team 

Test Conductor 

Technicians 

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4.13.4.1 Continued 

Quality Assurance Init 

AFQA Init 

Aerospace Observer Init 

AFSO Init 

4.13.5 Verification Test Procedure 

4.13.5.1 Verify by Inspection of Quality Assurance Records 

that the Headrest conforms to SK56197-453 and 

attach the records to these data sheets. 

4.13.6 Demonstration Test Procedure 

None 

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4.14 Requirement Title: TARGET LOADING AND COORDINATION 

4.14.1 Requirement Paragraph in Test Requirements Document 

3.1.1.1.7.1.5 

4.14.2 Requirement 

Demonstrate target selection logic. 

4.14.3 Related Paragraph in System Test Plan 

4.14 

4.14.4 Pre-Test Requirements 

None 

4.14.5 Verification Test Procedure 

No Test required. Requirement will be demonstrated during DOP's. 

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4.15 Requirement Title: SCENE DYNAMICS 

4.15.1 Requirement Paragraph in Test. Requirements 

Document 

3.1.1.1.7.1.6 and 3.1.1.1.8.1.6 

4.15.2 Requirement 

Tests will be performed to determine the phase 

0 Capability. 

4.15.3 Related Paragraph in System Test Plan 

4.15 

4.15.4 Pre-Test Requirements 

4.15.4.1 Test Team 

Test Conductor Init 

Technicians 

Quality Assurance Init 

AFQA Init 

Aerospace Observer Init 

AFSO Init 

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4.15.4.2 Test Equipment Required 

1) Brush Mark 200B Analog Recorder or Equivalent 

2) T-Box S/N 4605- 

4.15.4.3 Equipment Confidence Status 

The Test Conductor will insure that all Test 

Equipment has a valid calibration sticker. 

Equipment Type Cal Date 

4.15.4.4 Subsystem Status 

The following are required to be active for 

this Test. 

ON OFF 

SCC X 

SLM X 

DIU X 

Stimulus S/S X 

Computer S/S X 

4.15.4.5 Power Turn On 

Turn Power On To all Subsystems 

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4.15.5 Verification Test Procedure 

4.15.5.1 The DOP for this Procedure will be an ATS 

Only DOP, consisting of 26 Groups, 1 Target 

per group. The script will contain the following Parameters. 

Stimulus Scale - 364,000:1 

Altitude - 75 NM 

Nadir Stimulus 

4.15.5.2 For verification of Requirement (Static Positioning Accuracy) the following errors will be inputed. 

Group 

1 

Target 

1 

Errors 

No Errors 

Target 

2 2 Latitude .1NM 

Location 

3 3 Longitude .1NM Errors 

4 4 Altitude .1NM 

5 5 Intrack .3NM 

Ephemeris 

6 6 Crosstrack .1NM 

7 7 Altitude .1NM Errors 

8 8 Roll 2 grri 

Attitude 

9 9 Pitch 2 Min 

10 10 Yaw 2 Min Errors 

4.15.5.3 Install leads at the A2 Power Conditioning to 

record the following: 

HPA X Position Drive 

HPA Y Position Drive 

HPA X FB 

HPA Y FB 

HPA Blank FB 

Channel Conn 

Jl-V Jl-W 

J1-X J1-y 

Jl-v J1-w 

J1.-x Jl-y 

J4-E J4-F 

4.15.5.4 Set Recorder chart speed at 20 MM/Sec. Turn 

On Recorders. 

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4.15.5.5 Activate the Resume Switch at the SCC. 

4.15.5.6 When Group 10, Target 10 is in view, activate 

Freeze and Stop the Recorders. 

4.15.5.7 Remove Recordings and attach to these Data Sheets. 

The Recording of the X and Y Feedback Signals (Output of Servo Positioning Potentiometer) will indicate 

actual Simulator Position for each error listed in 

4.15.5.2. A printout of a computer program which 

determines actual AVE pointing errors will be compared 

with the recordings to determine the Static Positioning accuracy. 

4.15.5.8 This portion of the Procedure will verify the Dynamic 

Positioning Accuracy. 

4.15.5.9 Install leads at the SVS Pwr Cond. to record the 

X and Y error signals. 

Channel 

X Error 

Y Error 

4.15.5.10 Activate the resume switch and start the Recorders. 

4.15.5.11 Manually point the Positioner during the next 16 targets. 

4.15.5.12 When Group 26, Target 26 is in view, stop the recorders and complete the DOP. 

4.15.5.13 Remove the recordings and attach to these Data Sheets. 

The comparison of the Drive Signals, both X and Y, 

with the error voltage (output of the Servo Summing 

Amplifier) will indicate the maximum dynamic positioning error. 

4.15.5.14 Attach the SVS Acceptance Test Data for minimum 

Step response to these Data Sheets. 

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4.16 Requirement Title: LIGHTING 

4.16.1 Requirement Paragraph in Test Requirements Document 

3.1.1.1.7.2.1 

4.16.2 Requirement 

Demonstrate that scene illumination can be varied from 

target to target. 

4.16.3 Related Paragraph in System Test Plan 

4.16 

4.16.4 Pre-Test Requirements 

None 

4.16.5 Verification Test Procedure 

No Test required. Requirement will be demonstrated during DOP's. 

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4.17 Requirement Title: INITIAL TARGET LOCATION 

4.17.1 Requirement Paragraph in Test Requirements 

Document 

3.1.1.1.7.2.3 

4.17.2 Requirement 

It must be demonstrated that the simulator will 

accept stimulus material from the specified ranges 

LPA HPA 

Scale Range A 128,000:1 to 160,000:1 32,000:1 to 40,000:1 

Scale Range B 286,000:1 to 364,000:1 71,500:1 to 91,000:1 

taken at obliquities of + 15° in stereo angle and + 45

o 

in roll angle. The simulator shall adjust the scale of 

the scene along the intrack and crosstrack axes to scales 

representative of 75 to 85 nm altitude and initial target 

locations of + 45° to -40° intrack with roll angles of 

+ 10o of the inherent roll angle in the stimulus slide. 

It is a further condition that simulated scene roll 

angles shall be limited to + 40°, and also that forward 

intrack obliquity of up to + 60° can be simulated with 

stimulus material of + 15

o or less stereo angle when the 

scale of the stimulus is such that the dimensionally 

adjusted ground scene is contained in the 9" x 9" 

stimulus slide.. 

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4.17 Requirement Title: INITIAL TARGET LOCATION CONTINUED 

4.17.3 Related Paragraph in System Test Plan 

4.17 

4.17.4 Verification Test Procedure 

The three components in the optical system of the 

simulator which have limited ranges of operation 

are: the anamorphic lenses, zoom lens, and K-rotator. 

The anamorphs can move through angles of -105° to 

+105°. The zoom magnifications can range from .09X 

to .56X. The K-rotator can operate from -180° to 

+180°. This analysis will determine what combinations 

of stimulus/simulation conditions constitute worst 

cases for each component individually. Then the anamorph and K-rotator angles and zoom magnifications will 

be calculated for these worst cases, and they will be 

compared to hardware limits. 

The anamorphic lenses will be exercised to extremes 

if the simulated scene is to appear at opposite orientation from the stimulus scene. That is - one of the 

worst case anamorph angles will occur when stimulus 

angles are +15° stereo, -35° obliquity, and simulation 

angles are -40° stereo, -35° obliquity. 

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MN h2 sim 

(cos Cc`N . S im ) 3/2 

cos N stim 

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4.17.4 Continued 

The anamorph angles are determined by the following 

set of equations: 

01 = ( 4 - 450 - ) - (9/2 

02 = ( f - 45° - ) + (912 

Where sinf) = 2/3 ( 1 ) 

cos 1 

tan (p= sin (9' cos C9- 

+ sin2+ )16 

cos o< = cos cos _a_ 

( 0( is aspect angle, = stereo, = obliquity 

rand A are determined using a computer program because of the complexity of calculation) 

A ratio of zoom magnifications is calculated by: 

where MO= zoom mag at Oessim 

MN= zoom mag at nadir 

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4.17.4 Continued 

The maximum zoom magnification ratio occurs when 

hIstim,= 85 nm, hsim= 75 nm, = 0°, Xstim = 

17.920 (Z.= +150,..2.= +100). This ratio can be 

converted to a zoom mag. range when MNis defined. 

The worst case derotation angle will be determined 

by: 

°D = ( LJ - 2 V)) 

when the corresponding values of 4 and 0 are discovered with aid of the computer. 

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4.18 Requirement Title: DYNAMIC TARGET LOCATION 

4.18.1 Requirement Paragraph in Test Requirements Document 

3.1.1.1.7.2.4 

4.18.2 Requirement 

Demonstrate that the stimulus subsystem (Paragraph 3.3.2) 

can simulate the apparent dynamic perspective, orientation, 

and slant range of the target, in real time, from the initial 

intrack position to 400 aft and that the simulator will accomplish the changes in scene appearance for both circular 

and elliptical orbits within the 75 to 85 nm band. 

4.18.3 Related Paragraph in System Test Plan 

4.18 

4.18.4 Pre-Test Requirements 

None 

4.18.5 Verification Test Procedure 

No Test required, Requirement will be demonstrated during DOP's. 

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4.19 Requirement Title: SCAN AREA 

4.19.1 Requirement Paragraph in Test Requirements Document 

3.1.1.1.7.2.5 

4.19.2 Requirement 

Demonstrate that line of sight excursions are limited only 

by the stimulus material format size. 

4.19.3 Related Paragraph in System Test Plan 

4.19 

4.19.4 Pre-Test Requirements: 

None 

4.19.5 Verification Test Procedure 

No test required. Test conducted under 4.36 will verify 

this Requirement. Requirement will be demonstrated during 

DOP. 

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4.20 Requirement Title: SCENE STREAMING 

4.20.1 Requirement Paragraph in Test Requirements Document 

3.1.1.1.7.2.6 

4.20.2 Requirement 

Demonstrate that the ground scene is blocked from view 

during periods of ATS slew, and that the field of view 

is illuminated at an intensity comparable to the scene 

intensity at these times. 

4.20.3 Related Paragraph in System Test Plan 

4.20 

4.20.4 Pre-Test Requirements 

None 

4.20.5 Verification Test Procedure 

No Test required. Requirement will be demonstrated during DOP's. 

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4.21 Requirement Title: CONTROL STICK AND MAGNIFICATION CONTROL DURING 

FREEZE 

4.21.1 Requirement Paragraph in Test Requirement Document 

3.1.1.1.7.4 

4.21.2 Requirement 

Demonstrate that, at the option of the SCC operator, the 

pilot can scan the stimulus and change magnification during 

the freeze mode. 

4.21.3 Related Paragraph in System Test Plan 

4.21 

4.21.4 Pre-Test Requirements 

None 

4.21.5 Verification Test Procedure 

No Test Required. Test conducted under 4.33 will verify 

this requirement. Requirement will be demonstrated during 

DOP. 

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4.22 Requirement Title: MAGNIFICATION AND REAL FIELD OF VIEW 

4.22.1 Requirement Paragraph in Test Requirements Document 

3.1.1.1.8.1.1 

4.22.2 Requirement 

Demonstrate that the simulator will accomplish simulated 

magnification step changes between the values of 125X, 

and between the values of 

Demonstrate that 

the real field of view is 0.32 degree + 5% at 125X and 

that is varies inversely with magnification. 

4.22.3 Related Paragraph in System Test Plan 

4.22 

4.22.4 Pre-Test Requirements 

4.22.4.1 Test Team 

Test Conductor Init 

Technicians 

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4.22.4.1 Continued 

Quality Assurance Init 

AFQA Init 

Aerospace Observer Init 

AFSO Init 

4.22.4.2 Test Equipment Required 

1) Techniwrite Model TR6460, Event Recorders or 

equivalent 

2) Brush Mark 200B Analog Recorder or equivalent 

4.22.4.3 Equipment Confidence Status 

The Test Conductor will insure that all Test 

Equipment has a valid calibration sticker 

Equipment Type Cal Date 

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4.22.4.4 Subsystem Status 

The following are required to be active during 

this Test. 

ON OFF 

SCC X 

SLM X 

DIU 

Stimulus S/S X 

4.22.4.5 Power Turn On 

1) Turn Power on to all subsystems 

4.22.5 Verification Test Procedure 

4.22.5.1 Install Patchcords at the System Junction Box 

to record the following: 

Channel 

MO HAG (125X) 

4.22.5.2 Install Leads at the A2 

Power Conditioning to record the following. 

Channel 

LPA Spherical Zoom Drive 

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4.22.5.3 An analysis (similar to 4.12) has been performed 

q to relate Stimulus Scale Factor to required 

magnifications and determine the required drive 

voltage to simulate 125X 

4.22.5.4 Load an ATS/MO or MO only DOP into the SDS 930 

Computer. 

4.22.5.5 Turn on all devices for LPA and activate resume. 

4.22.5.6 Set the Magnification Stick to MO (125X). 

4.22.5.7 Set the Magnification Stick to 

4.22.5.8 Set the Magnification Stick to 

4.22.5.9 Set the Magnification Stick to 

4.22.5.10 Activate Freeze 

4.22.5.11 Remove recordings and attach to these data sheets 

for review with the analysis and SVS Zoom Calibration 

data to verify that the drive voltages specified in 

the analysis and SVS data are achieved within + 5%. 

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Page 54 

4.23 Requirement Title: EYEPIECE PROPERTIES 

4.23.1 Requirement Paragraph in Test Requirements Document 

3.1.1.1.8.1.2 

4.23.2 Requirement 

The eyepiece properties will be those for the acquisition 

subsystem with the exception that the image will be masked 

down to a 40° + 1° apparent field of view. The apparent 

field of view will be demonstrated. 

4.23.3 Related Paragraph in System Test Plan 

4.23 

4.23.4 Pre-Test Requirements 

4.23.4.1 Test Team 

Test Conductor 

Technicians 

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4.23.4.1 Continued 

Quality Assurance Init 

AFQA Init 

Aerospace Observer Init 

AFSO Init 

4.23.4.2 Test Equipment Required 

1) Spectra Pritchard Photometer - Model 1970 PR 

2) Photometer Mount 

4.23.4.3 Equipment Confidence Status 

The Test Conductor will insure that all Test Equipment has a valid cablibration sticker. 

Equipment Type Cal Date 

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4.23.4.4 Subsystems Status 

The following are required to be active during 

this Test 

ON OFF 

SCC X 

SLM X 

DIU X 

Stimulus S/S X 

Computer S/S X 

4.23.4.5 Power Turn On 

1) Turn power on to all subsystems except 

the DIU. 

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4.23.5 Test Procedure 

4.23.5.1 At the SCC Panel 2A, verify that the Servo 

Test Switch is not activated. 

4.23.5.2 Turn on the LPA Light Source and LPA Spherical 

Zoom. Activate the Selector to LPA and unblank 

LPA. Insert the 40° mask in the LPA Reticle Plane. 

4.23.5.3 Attach the Photometer Mount and Photometer to the 

supplemental Eyepiece. 

4.23.5.4 Locate the center of the Photometer Spot on the 

Left Hand Edge of the Field of View and record 

the angle from the Normal. 

Degrees 

4.23.5.5 Locate the Spot at the Right Hand Edge of the FOV 

and record the Angle from Normal. 

Degrees 

The Sum of the Two Angles should be 40° + 10. 

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4.24 Requirement Title: PERIPHERAL DISPLAY 

4.24.1 Requirement Paragraph in Test Requirements Document 

3.1.1.1.8.1.2.1 

4.24.2 Requirement 

The VO peripheral display will be incorporated in the ATS 

pattern. The 32 timer lights will appear on the left 

hand side of the display. 

4.24.3 Related Paragraph in System Test Plan 

4.24 

4.24.4 Pre-Test Requirements: 

None 

4.24.5 Verification Test Procedure 

No Test required. Requirement will be demonstrated during DOP's. 

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4.25 Requirement Title: TARGET COORDINATION AND LOADING 

4.25.1 Requirement Paragraph in Test Requirements Document 

3.1.1.1.8.1.5 

4.25.2 Requirement 

It will be shown that targets selected by voting logic 

during the ATS/MO mode demonstration shall be available 

for viewing through the eyepiece for MO in the appropriate 

time sequence. The target will appear at a time corresponding to the end of slew and remain in view until the 

commencement of slew to the next target. 

4.25.3 Related Paragraph in System Test Plan 

4.25 

4.24.4 Pre-Test Requirements: 

None 

4.25.5 Verification Test Procedure 

No Test required. Requirement will be demonstrated during 

DOP'S. 

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4.26 Requirement Title: SCENE LIGHTING 

4.26.1 Requirement Paragraph in Test Requirement Document 

3.1.1.1.8.2.1.2 

4.26.2 Requirement 

It will be demonstrated that the scene brightness will be 

variable over a range of 50:1 + 10% up to 20 + 2 foot 

lamberts as seen by the operator with no stimulus slide 

• in the optical path. 

4.26.3 Related Paragraph in System Test Plan 

4.26 

4.26.4 Pre-Test Requirements 

4.26.4.1 Test Team 

Test Conductor Init 

Technicians 

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4.26.4.1 Continued 

Quality Assurance Init 

AFQA Init 

Aerospace Observer Init 

AFSO Init 

4.26.4.2 Test Equipment Required 

1) Spectra Pritchard Photometer - Model 1970-PR 

2) Photometer Mount 

4.26.4.3 Equipment Confidence Status 

The Test Conductor will insure that all Test 

equipment has a valid calibration sticker. 

Equipment Type Cal Date 

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4.26.4.4 Subsystems Status 

The following are required to be active during 

this Test. 

ON OFF 

SCC X 

SLM X 

DIU X 

Stimulus S/S X 

Computer S/S X 

4.26.4.5 Power Turn On 

1) Turn power on to all subsystems except the 

DIU. 

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Page 63 

4.26.5 Test Procedure 

4.26.5.1 Verify that there is no Slide in the LPA 

Viewing Station and that the SVS Reticle is 

not is place. 

4.26.5.2 At the SCC Panel 2A, verify that the Servo Test 

Switch is activated and select the LPA Filter 

Modulator Servo Test. 

4.26.5.3 Attach the Photometer Mount and Photometer 

to the Supplemental Eyepiece. 

4.26.5.4 Turn On the LPA Light Source, activate the 

Selector to HPA and Unblank LPA. Center the 

Photometer Spot on the approximate center of the 

field. 

4.26.5.5 Set the LPA filter modulator servo test control 

to maximum (+50 V) and measure and record the 

system brightness. 

Foot Lamberts 

4.26.5.6 Set the LPA filter modulator servo test control 

to minimum (-50 V) and measure and record the 

system brightness. 

Foot Lamberts 

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4.26.5.7 Calculate the brightness range 

Max = Ratio 

Min 

4.26.5.8 Calculate the quantity and density of Wrotten 

Neutral Density filters required to reduce 

the brightness to approximately 0 to 20 foot 

lamberts. 

4.26.5.9 Insert the required filters and adjust the 

fixed filter at the LPA filter modulator 

until the brightness is between 18 and 22 

foot lamberts. 

4.26.5.10 Attach calibration data from SVS Acceptance 

to show the relationship between Computer 

Commands and Output Brightness to these data 

sheets. 

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4.27 Requirement Title: TARGET LOCATION RELATIVE TO VEHICLE 

4.27.1 Requirement Paragraph in Test Requirements Document 

3.1.1.1.8.2.3 

4.27.2 Requirement 

Show that targets within the envelope of: 

30 degrees forward to 40 degrees aft in track, 

40 degrees left to 40 degrees right crosstrack, 

and 75 to 85 nm altitude 

can be simulated. Perspective and slant range associated 

with the above envelope are considered to be properties 

of the stimulus material and will not be altered by the MDS. 

Show that altitudes beyond the range stated are possible if 

proper stimulus material is provided with scale factor proportional to the required altitude. 

Show that the in-track line on the ground scene is properly 

oriented for each target and fixed in time. This orientation shall be determined by the script depending on 

the status of the derotation prism, orbit inclination and 

target latitude. 

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4.27.3 Related Paragraph in System Test Plan 

4.27 

4.27.4 Pre-Test Requirements: 

None 

4.27.5 Verification Test Procedure 

No Test required. Requirement will be demonstrated during 

DOP's. 

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Page 67 

THIS TEST IS NOT REQUIRED. THE TEST PERFORMED UNDER 4.12.5.23 THRU 

4.12.5.27 WILL VERIFY THIS REQUIREMENT 

4.28 Requirement Title: SOURCE HOLDING AND SELECTION SYSTEM 

4.28.1 Requirement Paragraph in Test Requirement Document 

3.3.2.1.2 

4.28.2 Requirement 

1) The adjacent slide position to the one in viewing 

position may be selected and viewed within one 

second. 

2) The changer may be commanded to any diapositive, forward or reverse of the present position, and to 

operate the two elevators independently. 

4.28.3 Related Paragraph in System Test Plan 

4.28 

4.28.4 Pre-Test Requirements 

4.28.4.1 Test Team 

Test Conductor Init 

Technicians 

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4.28.4.1 Continued 

Quality Assurance Init 

AFQA Init 

Aerospace Observer Init 

AFSO Init 

4.28.4.2 Test Equipment Required 

1) Techniwrite Model TR6460, Event Recorders 

or equivalent. 

4.28.4.3 Equipment Confidence Status 

The Test Conductor will insure that all Test 

Equipment has a valid calibration sticker. 

Equipment Type Cal Date 

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4.28.4.4 Subsystems Status 

The following are required to be active during 

this Test. 

ON OFF 

SCC X 

SLM X 

DIU X 

Stimulus S/S X 

Computer S/S X 

4.28.4.5 Power Turn On 

1) Turn Power On to all Subsystems except the 

SLM. 

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4.28.5 Verification Test Procedure 

4.28.5.1 Turn on the HPA and LPA Holder Changers 

4.28.5.2 Load special Program No. 1 into the SDS 930 

Computer. 

4.28.5.3 Install Patchcords at the System Junction Box 

to record the following signals (if Patchcords 

are installed, verify recorder channels. 

HPA LPA 

Supply Elevator Raise 26 3 

Supply Elevator Busy 27 4 

Supply Elevator Lower 28 6 

Transport Load 34 12 

Transport Recall 36 14 

Transport Busy 35 13 

Takeup Elevator Raise 30 8 

Takeup Elevator Lower 32 10 

Takeup Elevator Busy 31 9 

Blanking Cmd 37 15 

Blanking Feedback 38 16 

4.28.5.4 Set the Recorder Chart Speed at 20MM/Sec and 

turn On the Recorders. 

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4.28.5.5 Activate the Computer Start Switch to initiate 

commands to the HPA Supply Elevator Raise and 

Transport Load Lines. Record the elapsed 

time from initiation of Raise Command to the 

Shutter Unblank. As indicated by the change in 

Level of the HPA Blanking FB. 

Sec Req is 1.0 Sec or Less. 

4.28.5.6 Repeat for HPA Supply Elevator Lower and Transport Load Lines. 

Sec Req is 1.0 Sec. or Less. 

4.28.5.7 Repeat of HPA Takeup Elevator Raise and Transport Recall Lines. 

Sec Req is 1.0 Sec. or Less. 

4.28.5.8 Repeat for HPA Takeup Elevator Lower and Transport Recall Lines. 

Sec Req is 1.0 Sec. or Less. 

4.28.5.9 Repeat for LPA Supply Elevator Raise and Transport Load Lines. 

Sec Req is 1.0 Sec. or Less. 

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4.28.5.10 Repeat for LPA Supply Elevator Lower and 

Transport Load Lines. 

Sec Req is 1.0 Sec. or less 

4.28.5.11 Repeat for LPA Takeup- Elevator Raise and 

Transport Recall Lines. 

Sec Req is 1.0 Sec. or Less. 

4.28.5.12 Repeat for LPA Takeup Elevator Lower and 

Transport Recall Lines. 

Sec Req is 1.0 Sec. or Less. 

4.28.5.13 Remove Recordings and Attach to these Data 

Sheets. 

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THIS TEST IN NOT REQUIRED. THE TEST PERFORMED UNDER 4.12.5.28 AND 

4.12.5.29 WILL VERIFY THIS REQUIREMENT. 

4.29 Requirement Title: SOURCE HOLDING AND SELECTION SYSTEM 

4.29.1 Requirement Paragraph in Test Requirement Document 

3.3.2.1.2 

4.29.2 Requirement 

It shall be demonstrated that five slide positions can 

be skipped and a slide from the sixth position can be 

viewed in 3 seconds or less. 

4.29.3 Related Paragraph in System Test Plan 

4.29 

4.29.4 Pre-Test Requirements 

4.29.4.1 Test Team 

Test Condutor 

Technicians 

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4.29.4.1 Continued 

Quality Assurance Init 

AFQA Init 

Aerospace Observer Init 

AFSO Init 

4.29.4.2 Test Equipment Required 

1) Techniwrite Model TR6460, Event Recorders 

or equivalent. 

4.29.4.3 Equipment Confidence Status 

The Test Conductor will insure that all Test 

Equipment has a valid calibration sticker. 

Equipment Type Cal Date 

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4.29.4.4 Subsystems Status 

The following are required to be active 

during this Test. 

ON OFF 

SCC X 

SLM X 

DIU X 

Stimulus S/S X 

Computer S/S X 

4.29.4.5 Power Turn On 

1) Turn Power On to all Subsystems except 

the SLM. 

4.29.5 Verification Test Procedure 

4.29.5.1 Turn on the HPA and LPA Holder Changer. 

4.29.5.2 Load Special Program No. 2 into the SDS 930 

Computer. 

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4.29.5.3 Install Patchcords at the System Junction Box to 

to record the following Signals (If Patchcords are 

installed, verify recorder channels) 

Channels 

HPA LPA 

Supply Elevator Lower 28 

Supply Elevator Busy –22.— __A__ 

Transport Load 

Transport Busy 

Takeup Elevator Lower 

Takeup Elevator Busy 

Transport Recall 

Blanking CMD 

Blanking Feedback 

4.29.5.4 Set the Recorder Chart Speed at 20 MM/Sec and 

turn On the Recorders. 

4.29.5.5 Activate the Computer Start Switch in Initiate Commands to the HPA Supply Elevator Lower and Transport Load Lines to skip 5 Slide Positions and Load 

the sixth. Record the elapsed time from initiation 

of Lower Command to Shutter Unbiank as indicated 

by the change in Level of the Blanking Feedback. 

Sec Req is 3.0 Sec or Less 

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4.29.5.6 Repeat for HPA Takeup Elevator Lower and 

Transport Recall Lines. 

Sec Req is 3.0 Sec or Less 

4.29.5.7 Repeat for LPA Takeup Elevator Lower and 

Transport Recall Lines. 

Sec Req is 3.0 Sec or less 

4.29.5.8 Repeat for LPA Supply Elevator Lower and 

Transport Load Lines. 

Sec Req is 3.0 Sec or Less. 

4.29.5.9 Remove Recordings and attach to these Data 

Sheets. 

4.29.6 Demonstration Test Procedure 

None 

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4.30 Requirement Title: IMAGE INTENSITY 

4.30.1 Requirement Paragraph in Test Requirements Document 

3.3.2.1.3.1 

4.30.2 Requirement 

It will be demonstrated that the color balance of the 

light is between 30000 and 6000° Kelvin. 

It will be demonstrated that: 

1) The image intensity can be varied through a range 

of 50:1 with the upper level 500 foot lamberts +10%. 

2) The intensity of the image 5 degrees from the edge 

is no less than 50 percent of the on axis intensity. 

NOTE: These numbers will be measured at the eyepiece 

without diapositives in the holder. 

3) The color change shall not vary more than + 25 

mireds over the intensity range. 

4.30.3 Related Paragraph in System Test Plan 

4.30 

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4.30.4 Pre-Test Requirements: 

None 

4.30.5 Verification Test Procedure 

No Test required. The SVS Acceptance Test Data verifying 

these Requirements shall be attached to these Data Sheets. 

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4.31 Requirement Title: MANUAL FILTER WHEEL 

4.31.1 Requirement Paragraph in Test Requirement Document: 

3.3.2.1.3.2 

4.31.2 Requirement 

It will be demonstrated that the manual filter wheel insertion 

simulated the optical path transmittances at 100%, 507. and 25%. 

Furthermore, it will be demonstrated that it is readily possible 

to change these transmittances to other values. 

4.31.3 Related Paragraph in System Test Plan: 

4.31 

4.31.4 Pre-Test Requirements 

4.31.4.1 Test Team 

Test Conductor 

Technicians 

Init. 

Quality Assurance 

AFQA 

Aerospace Observer 

Init. 

Init. 

Init. 

AFSO 

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4.31.4.2 Test Equipment Required 

1) Spectra Pritchard Photometer - Model 1970-PR 

2) Photometer Mount 

4.31.4.3 Equipment Confidence Status 

The Test Conductor will insure that all test equipment 

has a valid calibration sticker. 

Equipment Type Cal,. Date 

4.31.4.4 Subsystem Status 

The following are required to be active during this 

test: 

ON 

SCC X 

SLM X 

DIU X 

STIMULUS S/S X 

COMPUTER S/S X 

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4.31.4.5 Power Turn On 

1) Turn Power On to all Subsystems. 

4.31.5 Test Procedure 

4.31.5.1 Attach the Photometer Mount and Photometer to 

the Supplemental Eyepiece and verify that the 

SVS Reticle is in Place. 

4.31.5.2 Remove all Magazines from Both Legs of the SVS. 

4.31.5.3 Turn on all Stimulus Subsystem devices except 

Reticle Light Source, Haze Light Source, and the 

Wipeout Display, and verify that the Manual Filter 

Wheel Setting is 1.0. 

4.31.5.4 Load the Program into the SDS 930 Computer. 

4.31.5.5 Activate the Resume Switch and after the Reticle 

is in view, activate Freeze. 

4.31.5.6 Center the Photometer on the Reticle Center, 

lock in place and measure and record the system 

brightness. 

Foot-Lamberts 

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4.31.5.7 Change the Manual Filter Wheet setting to 0.5, 

activate the Resume Switch and within approximately 

2.0 seconds, activate Freeze. 

4.31.5.8 Measure and record the system brightness 

Foot-Lamberts 

The brightness should be 40% to 50% of that measured 

in 4.31.5.5 

4.31.5.9 Change the Manual Filter Wheel setting to 0.25, 

activate the Resume Switch and within approximately 

2.0 seconds, activate Freeze. 

4.31.5.10 Measure and record the system brightness. 

Foot-Lamberts 

The brightness should be 22.5% to 27.5% of that measured 

in 4.31.5.5 

4.31.5.11 The Software Part 2 Specification Sections involving 

transmittance value changes shall be attached to 

these Data Sheets. 

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4.32 Requirement Title: IMAGE SIZE 

4.32.1 Requirement Paragraph in Test Requirements Document 

3.3.2.1.3.4 

4.32.2 Requirement 

It will be demonstrated that the angular magnification is by 

continuous zoom techniques. 

It will be demonstrated that: 

1. The magnification has a range of 7.2:1 

2. The field of view subtends an apparent 60 degrees + 1 degree 

at the eye. 

3. Lowest power the exit pupil is 4 mm + 0.2 mm 

4. Highest power the exit pupil is 2 mm + 0.1 mm 

5. The exit pupil size will vary inversely with magnification 

within the limits of item 3 and 4 above. 

6. Manual focus will have ± 3 diopter adjustment. 

4.32.3 Related Paragraph in System Test Plan 

4.32 

4.32.4 Pre-Test Requirement: 

None 

4.32.5 Verification Test Procedure 

4.32.5.1 No test required. The SVS acceptance test data 

verifying the requirements shall be attached to these 

data sheets. 

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4.33 Requirement Title: RESOLUTION REQUIREMENT 

4.33.1 Requirement Paragraph in Test Requirement Document 

3.1.2.1.3.5 

4.33.2 Requirement 

It will be demonstrated that when using a standard white 

on black bar chart of 2:1 contrast as an input, the 

device when simulating 127X at nadir from orbit shall 

provide at least 30 LP/mm for 32K scale stimulus and 67 

LP/mm for 72K scale stimulus. This performance shall be 

provided on axis as viewed through the supplemental eyepiece by the unaided eye, with optical drives operating, 

the target centered in the FOV and scene drifts nulled 

by the computer. The resolution variation from the center to the edge of the apparent field shall not vary by 

more than a factor of 2 from the on axis performance. 

The resolution under the above conditions shall not degrade by more than a factor of 2 from the performance at 

a simulated 127X where the device is configured to 

simulate a magnification of 63.5X. 

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4.33.3 Related Paragraph in System Test Plan 

4.33 

4.33.4 Pre-Test Requirements 

4.33.4.1 Test Team 

Test Conductor Init 

Technicians 

Quality Assurance Init 

AFQA Init 

Aerospace Observer Init 

AFSO Init 

4.33.4.2 Test Equipment Required 

1) Resolution Slide #14126803 

2) Eng. Test Box SK56179-999 

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4.33.4.3 Equipment Confidence Status 

The Test Conductor will insure that all Test 

Equipment has a valid calibration sticker. 

Equipment Type CAL Date 

4.33.4.4 Subsystems Status 

The following are required to be active 

during this Test. 

ON OFF 

SCC X 

SLM X 

DIU X 

Stimulus S/S X 

Computer S/S X 

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Page 88 

4.33.4.5 Power Turn On 

1) Turn Power On to all Subsystems, indicated in 

4.33.4.4 

4.33.5 Test Procedure 

4.33.5.1 Turn On the HPA and LPA positioners and Spherical 

Zooms. 

4.33.5.2 Connect the Eng. Test Box per SK56179-999. Select 

HPA and Unblank HPA. 

4.33.5.3 Insert the Resolution Slide in the HPA Viewing 

Station. 

4.33.5:4 Set the Spherical Zoom Drive Voltage at +33.24 V 

(127X) and center the Reticle on the ON axis Resolution Chart. Record the Readings from three 

qualified observers for 127X. For the positions 

indicated on the attached Data Sheets set the 

Spherical Zoom Drive Voltage at +0.38 V (63.5X) 

and center the Reticle on the On Axis Resolution Chart. 

Record the Readings from three qualified observers 

for 63.5X for the positions indicated on the attached 

data sheets. 

4.33.5.5 Remove the HPA High Power Arm and insert the Low 

Power Arm and repeat all Readings from 4.33.5.4 

SZ Voltage (127X) +38.88V 

(63.5X) + 8.59V 

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Page 89 

4.33.5.6 Activate the Selector to LPA, Blank HPA 

and Unblank LPA. Repeat all Readings from 

4.33.5.4 

SZ Drive Voltage (127X) +36.56V 

(63.5X) + 4.85V 

4.33.5.7 Remove the LPA High Power Arm and insert the 

Low Power Arm and repeat all Readings. 

SZ Drive Voltage (127X) 442.32V 

(63.5X) +13.43V 

SECRET/DOR IAN 

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-Y HI 63.5X 17 

ON Axis LO 127X 30 

+X LO 127X 15 

-X LO 127X 15 

+Y LO 127X 15 

-Y LO 127X 15 

ON Axis LO 63.5X 15 

+X LO 63.5X 8 

-X LO 63.5X 8 

+y LO 63.5X 8 

-Y LO 63.5X 8 

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Page 92 

4.34 Requirement Title: FIELD CURVATURE 

4.34.1 Requirement Paragraph in Test Requirements Document 

3.3.2.1.3.6 

4.34.2 Requirement 

It will be demonstrated that the curvature of the apparent 

field from center to edge under static conditions at 1:1 

anamorph setting using the supplemental eyepiece is no 

greater than 3.5 diopters. 

4.34.3 Related Paragraph in System Test Plan 

4.34 

4.34.4 Pre-Test Requirements: 

None 

4.34.5 Verification Test Procedure 

4.34.5.1 No Test Required. The SVS Acceptance Test 

Data verifying this Requirement shall be 

attached to these Data Sheets. 

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Page 93 

4.35 Requirement Title: IMAGE PERSPECTIVE 

4.35.1 Requirement Paragraph in Test Requirements Document 

3.3.2.1.3.8 

4.35.2 Requirement 

The anamorphic optics, which provide image perspective 

by distorting an input to simulate various slant angles 

of view, will be demonstrated. 

4.35.3 Related Paragraph in System Test Plan 

4.35 

4.35.4 Pre-Test Requirements 

None 

4.35.5 Verification Test Procedure 

4.35.5.1 No Test required. The SVS Acceptance Test 

Data verifying this Requirement shall be 

attached to these Data Sheets. 

4.35.6 Demonstration Test Procedure 

4.35.6.1 No Test required. Demonstrated as part of 

4.17 and 4.18 

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Page 94 

4.36 Requirement Title: OPTICAL CENTER SELECTION 

4.36.1 Requirement Paragraph in Test Requirements Document 

3.3.2.1.3.9 • 

4.36.2 Requirement 

It will be demonstrated that the center of the optical 

axis can be continuously varied to at least + 4 inches 

in the two orthogonal directions with respect to the 

center of the diapositives. 

4.36.3 Related Paragraph in System Test Plan 

4.36 

4.36.4 Pre-test Requirements 

None 

4.36.5 Verification Test Procedure 

4.36.5.1 No Test required. The SVS Acceptance Test Data 

verifying this Requirement shall be attached 

to these Data Sheets. 

4.36.6 Demonstration Test Procedure 

None 

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Page 95 

4.37 Requirement Title: BRIGHTNESS CONTROL 

4.37.1 Requirement Paragraph in Test Requirements Document 

3.3.2.1.4.1 

4.37.2 It will be demonstrated for the filter modulator that: 

1) Any position within the brightness range can be 

set within 1 second. 

2) Control accuracy is within + 10 percent of a commanded foot lambert setting. 

4.37.3 Related Paragraph in System Test Plan 

4.37 

4.37.4 Pre-Test Requirements 

None 

4.37.5 Verification Test Procedure 

4.37.5.1 No Test required. The SVS Acceptance Test 

Data verifying this Requirement shall be 

attached to these Data Sheets. 

4.37.6 Demonstration Test Procedure 

None 

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4.38 Requirement Title: MAGNIFICATION CONTROL 

4.38.1 Requirement Paragraph in Test Requirements Document 

3.3.2.1.4.2 

4.38.2 Requirement 

It will be demonstrated that the spherical zoom control 

will cause any required 2:1 magnification change within 

0.5 seconds and will reset to any position within one 

second. Furthermore, it will be demonstrated that the 

control is continuous over the operating range as 

specified in paragraph (3.3.2.1.3.4). 

4.38.3 Related Paragraph in System Test Plan 

4.38 

4.38.4 Pre-Test Requirements 

None 

4.38.5 Verification Test Procedure 

4.38.5.1 No Test required. The measurements taken in 

4.12 and the SVS Acceptance Test Data verify 

this Requirement. Attach the SVS Acceptance 

Test Data to the Data Sheets. 

4.38.6 Demonstration Test Procedure 

None 

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4.39 Requirement Title: ANAMORPHIC CONTROL 

4.39.1 Requirement Paragraph in Test Requirement Document 

3.3.2.1.4.3 

4.39.2 Requirement 

It will be demonstrated that: 

1) Anamorphic azimuth is continuously variable from 0 to 

360 optical degrees. 

2) Positional accuracy is + 15 arc minutes. 

3) Any position can be accomplished within ,1 second. 

4.39.3 Related Paragraph in System Test Plan 

4.39 

4.39.4 Pre-Test Requirements 

4.39.4.1 Test Team 

Test Conductor 

Technicians 

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4.39.4.1 Continued 

Quality Assurance Init 

AFQA Init 

Aerospace Observer Init 

AFSO Init 

4.39.4.2 Test Equipment Required 

1) Brush Mark 200 B Analog recorder or 

equivalent. 

4.39.4.3 Equipment Confidence Status 

The Test Conductor will insure that all Test 

Equipment has a valid calibration sticker. 

Equipment Type Cal Date 

4.39.4.4 Subsystem Status 

The following are required to be active during 

this Test. 

ON OFF 

SCC X 

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4.39.4.4 Continued 

ON OFF 

SLM X 

DIU X 

Stimulus S/S X 

Computer S/S X 

4.39.4.5 Power Turn On 

1) Turn Power On to all Subsystems. 

4.39.5 Verification Test Procedure 

4.39.5.1 No Test is required for Requirements 1 and 2. 

The SVS Acceptance Test Data verifying these 

Requirements shall be attached to these Data 

Sheets. 

4.39.5.2 Set Up two Switches at the Beckman 2200 to 

supply -50 VDC to +50 VDC Step Commands. 

One Switch shall provide the Step on T128 

(Signal) and T129 (Return). The other shall 

provide the Step on T130 (Signal) and T131 

(Return). 

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4.39.5.3 Install Leads at the A2 Power Conditioning 

SVS Interface Connector Jl and J2, to record the following: 

Channel Conn. 

HPA LPA HPA LPA 

Cyl Zoom 1/2X Drive Jl-h i J2-h i 

Cyl Zoom 1/2X FB Jl-DD EE J2-DD EE 

Cyl Zoom 2X Drive J1-1,k J2-j,k 

Cyl Zoom 2X FB Jl-FF GG J2-FF GG 

4.39.5.4 Turn On HPA and LPA Cyl Zoom 1 and 2. Set 

Recorder Chart Speed at 20 MM/Sec. Turn On 

Recorders. 

4.39.5.5 Activate both Switches at the Beckman 2200. 

Record the elapsed time from initiation of 

Step Command to Settling of the Feedback within + 10%, as indicated by the change in Feedback Polarity, for both HPA Cyl Zoom 1 and 2. 

Sec - HPA Cyl Zoom 1 

Sec - HPA Cyl Zoom 2 

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4.39.5.6 Change the Outputs at the Beckman 2200 

From T128 To T140 

T129 T141 

T130 T142 

T131 T143. 

4.39.5.7 Repeat 4.39.5.5 for LPA Cyl Zoom 1 and 1 

Sec - LPA Cyl Zoom 1 

Sec - LPA Cyl Zoom 2 

4.39.5.8 Remove recordings and attach to these Data 

Sheets. 

4.39.6 Demonstration Test Procedure 

None 

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4.40 Requirement Title: IMAGE ROTATION 

4.40.1 Requirement Paragraph in Test Requirements Document 

3.3.2.1.4.4 

4.40.2 Requirement 

It will be demonstrated that: 

1) The image rotation is continuously variable from 

0 to 360 degrees. 

2) Any position can be accomplished within 1 second. 

3) Positional accuracy is + 30 arc minutes. 

4.40.3 Related Paragraph in System Test Plan 

4.40 

4.40.4 Pre-Test Requirements: 

None 

4.40.5 Verification Test Procedure 

4.40.5.1 No Test required. The SVS Acceptance Test Data 

verifying this Requirement shall be attached 

to these Data Sheets. 

4.40.6 Demonstration Test Procedure 

None 

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4.41 Requirement Title: POSITION SELECTION 

4.41.1 Requirement Paragraph in Test Requirements Document 

3.3.2.1.4.5 

4.41.2 Requirement 

1) The center of the optics chain has a position accuracy 

of _ 0.0059 inches. 

2) Any position, within the operating range, has a repeatable accuracy of 0.0004 inches. 

The minimum position change is 0.0004 inches. 

4) The position change is capable of a change rate between 0 and 4.61 inches per second. 

5) During position change, position commands may contain accelerations between 0 and 38 inches per 

second squared. 

4.41.3 Related Paragraph in System Test Plan 

4.41 

4.41.4 Pre-Test Requirements 

None 

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4.41.5 Verification Test Procedure 

4.41.5.1 No Test required. The SVS Acceptance Test 

Data verifying this Requirement shall be 

attached to these Data Sheets. 

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4.42 Requirement Title: ACQUISITION PERIPHERAL DISPLAY 

4.42.1 Requirement Paragraph in Test Requirements Document 

3.3.2.1.4.6.1 

4.42.2 Requirement 

It will be demonstrated that: 

1) All peripheral lights are displayed against a dark 

background in the outer three degrees in the periphery 

of a 60 degree field of view. 

2) All lights subtend one-half degree in the field of view. 

3) All lights have the capability of being switched on 

singly, in any combination or sequence. 

4) There are 35 lights in the wipe out display and the 

design has a capacity for 45 lights. 

5) There are 25 lights equally spaced within a 120 degree 

arc in the left hand field of view 60 degrees above 

and 60 degrees below the horizontal centerline. 

6) There are 5 lights equally spaced and centered in a 

30 degree acr centered in the upper right quadrant. 

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4.42.2 Requirement (Continued) 

7) There are 5 lights equally spaced and centered in a 

30 degree arc centered in the lower right quadrant. 

8) There is a means provided to color the peripheral 

lights individually. 

9) There is sufficient flexibility to simulate a wide 

variety of potential AVE configurations. 

4.42.3 Related Paragraph in System Test Plan 

4.42 

4.42.4 Pre-Test Requirements: 

None 

4.42.5 Verification Test Procedure 

4.42.5.1 Requirements 1 and 3 will be verified by 4.43 

Paragraph 4.43.5.3 

4.42.5.2 Attach Drawings 

To these Data Sheets, for a review to verify 

Requirements 2, 4, 5, 6, 7, 8, 9 

4.42.6 Demonstration Test Procedure 

None 

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4.43 Requirement Title: ACQUISITION PERIPHERAL DISPLAY 

4.43.1 Requirement Paragraph in Test Requirement Document 

3.3.2.1.4.6.1 

4.43.2 Requirement 

10) The brightness is variable over a 50:1 + 10% range. 

11) The maximum brightness is 500 foot lamberts + 10%. 

4.43.3 Related Paragraph in System Test Plan 

4.43 

4.43.4 Pre-Test Requirements 

4.43.4.1 Test Team 

Test Conductor 

Technicians 

Quality Assurance Init 

AFQA Init 

Aerospace Observer Init 

AFSO Init 

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4.43.4.2 Test Equipment Required 

1) Spectra Pritchard Photometer Model 1970-PR 

2) Photometer Mount SK 

4.43.4.3 Equipment Confidence Status 

The Test Conductor will insure that all Test 

Equipment has a valid calibration sticker. 

Equipment Type Cal Date 

4.43.4.4 Subsystem Status 

The following are required to be active during 

this Test. 

ON OFF 

SCC X 

SLM X 

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4.43.4.4 Continued 

ON OFF 

DIU X 

Stimulus S/S X 

Computer S/S X 

4.43.4.5 Power Turn On 

1) Turn Power On to all Subsystems except 

the DIU. 

4.43.5 Test Procedure 

4.43.5.1 At the SCC Panel 2A, verify that the Servo 

Test Switch is not activated. 

4.43.5.2 Attach the Photometer Mount and Photometer 

to the Supplemental Eyepiece. 

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4.43.5.3 Turn On all Wipeout Lights singly and unblank the 

Wipeout Display. Verify that all other Light 

sources are Off. 

4.43.5.4 Set the Wipeout Brightness Control to maximum, 

and center the Photometer spot on one of the 

Wipeout Lights. Measure and record the Brightness. 

4.43.5.5 Set the Wipeout Brightness Control to minimum. 

Measure and record the Brightness. 

4.43.5.6 Repeat 4 and 5 for two more Wipeout Lights 

Mlx Ratio Light 1 

Min 

Max Ratio Light 2 

Min 

Max Ratio .Light 3 

Min 

Maximum shall be 450 to 550 foot Lamberts. Required 

Ratio is 45:1 to 55:1. 

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4.44 Requirement Title: HAZE REQUIREMENT 

4.44.1 Requirement Paragraph in Test Requirement Document 

3.3.2.1.4.6.2 

4.44.2 Requirement 

The haze brightness (atmospheric luminance) will be 

demonstrated to show that: 

1) The brightness is variable over a 50:1 + 10% range. 

2) The upper level is 500 foot lamberts + 10%. 

4.44.3 Related Paragraph in System Test Plan 

4.44 

4.44.4 Pre-Test Requirements 

4.44.4.1 Test Team 

Test Conductor Init 

Technicians 

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4.44.4.1 Continued 

Quality Assurance Init 

AFQA Init 

Aerospace Observer Init 

AFSO Init 

4.44.4.2 Test Equipment Required 

1) Spectra Pritchard Photometer Model 1970-PR 

2) Photometer Mount SK 

4.44.4.3 Equipment Confidence Status 

The Test Conductor will insure that all Test 

Equipment has a valid calibration sticker. 

Equipment Type Cal Date 

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4.44.4.4 Subsystems Status 

The following are required to be active 

during this Test 

ON OFF 

SCC X 

SLM X 

DIU X 

Stimulus S/S X 

Computer S/S X 

4.44.4.5 Power Turn On 

1) Turn Power On to all Subsystems except 

the DIU. 

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4.44.5 Test Procedure 

4.44.5.1 At the SCC Panel 2A, verify that the Servo 

Test Switch is activated. 

4.44.5.2 Attach the Photometer Mount and Photometer to the 

Supplemental Eyepiece. 

4.44.5.3 Turn On the HPA Light Source, activate the Selector 

to HPA, Unblank HPA and select the Haze Filter Modulator Servo Test. Verify that all other Light 

Sources are Off. 

4.44.5.4 Center the Photometer Spot on the Reticle Center. 

4.44.5.5 Turn On the Haze Light Source and set the Haze 

Filter Modulator Servo Test Control at Maximum. 

4.44.5.6 Blank HPA and Unblank the Haze Light Source. Measure 

and record the Haze Brightness. 

Foot Lamberts 

450 to 550 Required 

4.44.5.7 Set the Haze Filter Modulator Servo Test Control to 

Minimum. Measure and record the Haze Brightness. 

Max 

Min 

Ratio 

Required Ratio is 45:1 to 55:1 

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4.45 Requirement Title: HAZE REQUIREMENT 

4.45.1 Requirement Paragraph in Test Requirements Document 

3.3.2.1.4.6.2 

4.45.2 Requirement 

The scene brightness and haze brightness will give proper 

appearance of the overall scene as seen from orbit. 

4.45.3 Related Paragraph in System Test Plan 

4.45 

4.45.4 Pre-Test Requirements 

None 

4.45.5 Verification Test Procedure 

4.45.5.1 No Test required. Requirement will be 

demonstrated during DOP'S. 

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4.46 Requirement Title: RETICLE REQUIREMENT 

4.46.1 Requirement Paragraph in Test Requirements Document 

3.3.2.1.4.6.3 

4.46.2 Requirement 

The reticle display will be demonstrated to show that: 

1) The brightness is variable over a 50:1 range within +107.. 

2) The upper level is 500 foot lamberts, + 107. 

4.46.3 Related Paragraph in System Test Plan 

4.46 

4.46.4 Pre-Test Requirements 

4.46.4.1 Test Team 

Test Conductor 

Technicians 

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4.46.4.1 Continued 

Quality Assurance Init 

AFQA Init 

Aerospace Observer Init 

AFSO Init 

4.46.4.2 Test Equipment Required 

1) Sprectra Pritchard Photometer Model 1970-PR 

2) Photometer Mount SK 

4.46.4.3 Equipment Confidence Status 

The Test Conductor will insure that all Test 

Equipment has a valid calibration sticker 

Equipment Type Cal Date 

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4.46.4.4 Subsystems Status 

The following are required to be active 

during this Test. 

ON OFF 

SCC X 

SLM X 

DIU X 

Stimulus S/S X 

Computer S/S X 

4.46.4.5 Power Turn On 

1) Turn Power On to all Subsystems except the DIU 

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4.46.5 Verification Test Procedure 

4.46.5.1 At the SCC Panel 2A, verify that the Servo Test 

Switch is not activated. 

4.46.5.2 Attach the Photometer Mount and Photometer to 

the Supplemental Eyepiece. 

4.46.5.3 Turn On the HPA Light Source, activate the Selector to HPA and Unblank HPA. Verify that all other 

Light Sources are Off. 

4.46.5.4 Center the Spot in the Photometer on the Reticle Center. 

4.46.5.5 Turn On the Reticle Light Source and set the Reticle 

Brightness Control to Maximum. 

4.46.5.6 Blank HPA and Unblank the Reticle. Measure and 

record the Reticle Brightness. 

Foot Lamberts 

450 to 550 Required 

4.46.5.7 Set the Reticle Brightness Control to Minimum. 

Measure and Record the Brightness. 

Max 

Min 

Ratio 

Required Ratio is 45:1 to 55:1 

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4.47 Requirement Title: RETICLE REQUIREMENT 

4.47.1 Requirement Paragraph in Test Requirements Document 

3.3.2.1.4.6.3 

4.47.2 Requirement 

It will be demonstrated that: 

1) The reticle is illuminated. 

2) The reticle will grow and contract with change in magnification. 

3) The reticle configuration can be changed. 

4.47.3 Related Paragraph in System Test Plan 

4.47 

4.47.4 Pre-Test Requirements 

None 

4.47.5 Verification Test Procedure 

4.47.5.1 No Test Required. Requirement will be 

demonstrated during DOP'S. 

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4.48 Requirement Title: CUE SUBSYSTEM 

4.48.1 Requirement Paragraph in Test Requirement Document 

3.3.2.1.4.6.4 

4.48.2 Requirement 

The Cue Subsystem will be presented by rear projection 

screen display on Panel 2C. Four operating modes shall 

be simulated in the rear projection display. 

1) Manual mode, single step 

2) Manual mode, random access 

3) Auto-Prepass Mode 

4) Auto-During Pass mode 

In the manual mode the ability to advance, backup, or random access shall be demonstrated. It shall be demonstrated 

that consecutive cues can be accessed in one second. Furthermore, it will be demonstrated that any cue in the cue 

file shall be accessible within 4 seconds. 

In the auto-prepass mode it will be demonstrated that 

the dwell time can be changed manually. 

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4.48.2 Requirement (Continued) 

Demonstrate that the auto-during pass mode will provide 

a computer controlled dwell time. 

It will be demonstrated that the cue system can provide 

the capability to present one cue per acquisition target in the during pass mode, and one cue of different 

content per acquisition target in the pre-pass mode. It 

will be further demonstrated that the cue film storage 

system uses 35 mm full frame slides with a holding capacity of 80 slides. 

4.48.3 Related Paragraph in System Test Plan 

4.48 

4.48.4 Pre-Test Requirements 

4.48.4.1 Test Team 

Test Conductor Init 

Technicians 

Quality Assurance Init 

AFQA Init 

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4.48.4.1 Continued 

Aerospace Observer Init 

AFSO Init 

4.48.4.2 Test Equipment Required 

1) Techniwrite Model TR6460 Event Recorders 

or equivalent. 

4.48.4.3 Equipment Confidence Status 

The Test Conductor will insure that all Test 

Equipment has a valid calibration sticker. 

Equipment Type Cal Date 

4.48.4.4 Subsystems Status 

The following are required to be active during 

This Test. 

ON OFF 

SCC X 

SLM X 

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4.48.4.4 Subsystems Status (Continued) 

ON OFF 

DIU X 

Stimulus S/S X 

Computer S/S X 

4.48.4.5 Power Turn On 

1) Turn Power On to all Subsystems. 

4.48.5 Verification Test Procedure 

4.48.5.1 Install Patchcords at the System Junction 

Box to record the following (If Patchcords 

are already installed, verify recorder 

channels). 

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4.48.5.1 Continued 

Channel 

Cue Go Cmd 41 

Cue Busy 42 

VDP Insert 49 

4.48.5.2 Load a DOP Program into the SDS 930 Computer. 

4.48.5.3 Verify that the VDP Pwr Switch at Panel 2D is 

"ON" and that the Frame Select is selecting 

Frame 1 (00001) 

4.48.5.4 Turn On the Cue Light Source and Projector. 

4.48.5.5 Activate the Resume Switch and Select Frame 2 

(00002). Activate the VDP Insert Switch. Activate the Freeze Switch when the Cue Requested 

Display indicates #2. 

4.48.5.6 Record the elapsed time from initiation of 

VDP insert to the change in Level of the Cue 

Busy. 

Sec Req is 1.0 Sec. 

4.48.5.7 Verify that the Cue Requested and Cue Selected 

Displays at the SCC Panel 5B are displaying 

Cue #2 Requested and Selected. 

Verified 

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4.48.5.8 Select Frame ( ), activate the Resume 

Switch and the activate the VDP Insert Switch. 

Activate the Freeze Switch when the Cue Requested display indicates # (Frame 

42 is 180° from Frame 2 and will require the 

longest access time.) 

4.48.5.9 Record the elapsed time from initiation of VDP 

Insert to the change in level of the Cue Busy. 

Sec Req is 4.0 Sec 

4.48.5.10 Verify that the Cue Requested and Cue Selected 

display at Panel 5B are displaying Cue # 

requested and selected. 

Verified 

4.48.5.11 Remove recordings and attach to these Data 

Sheets. 

4.48.5.12 This Procedure verifies only access times. 

The remainder of the requirement will be 

demonstrated during DOP. 

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5.0 DEMONSTRATION OF REQUIREMENTS 

This Section defined the Procedures to be used for conducting the Demonstration Orbital Passes (DOP'S). The script for each DOP will contain 

Stops before each target and/or Group of targets to allow for the Test 

Conductor to brief the AF Demonstration Team on the events occuring within the target or group, and to obtain agreement on the Requirements 

demonstrated by the preceding target or group. The following table lists 

the Requirements to be demonstrated during or prior to DOP'S and lists 

the paragraph number and type of DOP where the Requirement is demonstrated. 

paragraph 

4.1 

Pretest 

Checkout ATS Only ATS/MO 

5.1 

4.2 ' 5.1 5.2.7.7.26.1 5.4.6.4.8 5.3.6.2.26.2 

4.3 5.1 

4.4 5.2.7.7.26.1 

4.5 

4.6 5.2.7.7.27.1 5.3.6.3.27.1 

4.7 5.2.7.7.26.1 5.4.6.4.8 5.3.6.2.26.2 

4.8 No Demonstration Required 

4.9 5.2.7.5.1 

4.10 5.3.6.3.2.1 

4.11 5.3.6.3.26.1 

4.12 5.2.7.7.6.1 

4.13 No Demonstration Required 

4.14 5.4.6.4.8 

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5.0 CONTINUED 

Pretest 

Paragraph Checkout ATS Only ATS/MO MO 

4.15 5.2.7.7.26.1 5.4.6.4.8 5.3.6.3.26.3 

4.16 5.2.7.7.18.1 

4.17 5.2.7.7.10.1 5.3.6.3.26.1 

4.18 5.2.7.7.10.1 5.3.6.3.26.1 

4.19 5.2.7.7.19.1 

4.20 5.2.7.7.3.1 

4.21 5.2.7.7.1.1 5.3.6.3.3.1 

4.22 5.3.6.3.3.1 

4.23 

4.24 5.3.6.3.2.1 

4.25 5.4.6.4.8 

4.26 5.3.6.3.6.1 

4.27 5.3.6.3.26.1 

4.28 No Demonstration Required 

4.29 No Demonstration Required 

4.30 5.2.7.7.18.1 

4.31 5.2.7.7.19.1 

4.32 5.2.7.7.6.1 

4.33 5.2.7.7.19.1 

4.34 No Demonstration Required 

4.35 

4.36 5.2.7.7.19.1 

4.37 No Demonstration Required 

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5.0 DEMONSTRATION OF REQUIREMENTS (CONTINUED) 

Pretest 

Paragraph Checkout ATS Only ATS/MO MO 

4.38 No Demonstration Required 

4.39 1,1 11 It 

4.40 II II 11 

4.41 11 it 11 

4.42 It It It 

4.43 5.2.7.7.3.1 

4.44 5.2.7.7.14.1 

4.45 5.2.7.7.14.1 

4.46 5.2.7.7.1.1 

4.47 5.2.7.7.6.1 

4.48 5.2.7.7.3.1 5.2.7.5.1 

NOTE: The Demonstration of Requirements during DOP'S will be 

visual observations only. No physical measurements (such 

as Timing) will be made. All required physical measurements 

have been made under ection 4.0 (Verification of Requirements). 

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5.1 Pre-Test Checkout Program 

The Pre-Test Checkout Program Requirement will be demonstrated 

per Test Procedure BIN: BIF-055-46753-69 on the first day of 

Demonstration Tests, and at the option of the Test Conductor on 

the succeeding days. 

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5.2 ATS Only DOP 

5.2.1 General 

The test procedure for this DOP contains the tasks required to demonstrate specific requirements of the Phase 

0 NDS as defined in Section 4.0 of this Document. 

5.2.2 Requirements Demonstrated 

5.2.2.1 The following requirements will be demonstrated 

by the ATS only DOP prior to the Payload Pass. 

4.9 Event time operation 

4.48 (Partial) Cue Subsystem 

1) Manual callup 

2) Auto-prepass 

3) Alphanumeric Data 

The following requirements will be demonstrated 

during the Payload Pass. 

Group 1 4.20 Scene Streaming 

2 4.21 Control Stick and Magnification 

3 Control during Freeze 

4.42 Acquisition Peripheral Display 

4.48 Cue Subsystem (Auto During-Pass 

and Cue Hold) 

4.46 Reticle Req. 

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5.2.2.1 Continued 

Group 4 4.12 Magnification and Real FOV 

5 4.32 Image Size (Continuous Zoom) 

6 4.47 Reticle Requirement 

Group 7 4.17 Initial Target Location 

9 4.18 Dynamic Target Location 

Group 11 4.44 Haze Variation 

12 4.45 Haze (Haze and Scene Brightness 

Combined) 

13 

14 

Group 15 4.30 Image Intensity 

16 4.16 Lighting 

17 

18 

Group 19 4.31 Manual Filter 

4.33 Resolution 

4.36 Optical Center Selection 

4.19 Scan Area 

Group 20 thru 26 

4.11 Stick Input 

Group 1-26 

4.2 Controls and Displays 

4.7 Operations Scripting Capability 

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5.2.2.1 Continued 

Group 1-26 (Continued) 

4.15 Scene Dynamics 

4.16 10 Min Turn Around 

5.2.3 Scripting 

This DOP is scripted for both Primary Trackpath and ATS Trackpath #1 containing 26 groups of targets with a total of 58 

aiming points. The Primary Trackpath is contained in Trackpath 

1 and will be demonstrated. ATS Trackpath 2 will not be scripted 

or demonstrated. 

5.2.4 Stimulus 

The stimulus material for this DOP will be slides (LP, HP) numbered sequentially from 1 to 26, which will contain a grid of 

indexed intersections spaced on one inch centers across the 

format of each slide. 

Where resolution measurements are to be made, a slide with resolution targets (Tribar charts) will be substituted for the numbered 

gridwork slide. (These are identified in the Procedure). 

The cues for this DOP will be numbered 1 to 26 to correspond 

with group number. If more than one target is in a group, duplicate cue slides will be used. Each cue slide will contain the 

indexed intersection to be used as that target. 

5.2.5 Setup 

The MDS will be in an operational configuration as defined in the 

Pretest Checkout Procedure BIN:BIF-055-46753-69 with all simulation software and AVE programs loaded. 

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5.2.5 Continued 

The simulated command messages, stimulus data, and "SCRIPT" 

data will be read into the Computer Subsystem. The HP slides 

will be loaded in the HP arm of the SVS and the LP slides will 

in the LP arm, in accordance with the script slide load tables. 

The SLM setup will consist of a panel checklist for Panels 2C 

and 2D, contained in the Simulated VDP. 

For this DOP, the controls of interest and the positions selected 

are: 

Trackpath Select Primary Trackpath No. 1 

Magnification Controller LP Range 

VDP Command 

Right Hand Control Stick Centered 

5.2.6 Pre-Payload Pass Functions 

For this DOP, several tasks will be performed prior to actual 

start of the Payload Pass. These tasks are: 

1. Event Timer Setup 

2. Auto-Prepass Cue Briefing 

This will be an abbreviated briefing since the intent is to show 

the simulator capability to perform this task and not provide 

actual briefing for content. If Manual Single Step Mode is 

desired, place VDP Power Switch to "ON" and activate Single 

Step Switch. 

3. Manual Cue Callup 

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5.2.6 Continued 

This will require the crewman to callup and display the panel 

checklist for 2C and 2D prior to start of the Payload Pass. The 

intent here is to demonstrate the manual capability as well as 

provide the instructions for setting up the panels for the Payload Pass. 

5.2.7 ATS Only DOP Procedure 

5.2.7.1 General 

This DOP will commence when the "RESUME" command is 

initiated at the SCC. At this point, vehicle time for 

this DOP will be 112300 seconds. The MDS will be operating continuously through the end of the Payload Pass 

unless the "FREEZE" interrupt is initiated. 

Whenever the FREEZE is initiated the MDS is placed in 

a "hold" configuration until the "RESUME" is once more 

initiated. Then the MDS resumes operation from the point 

in time at which the FREEZE occurred. In order to have 

Control Stick and Magnification Control during FREEZE, the 

Stick FREEZE Switch at the SCC must be activated. 

One second prior to each Group Decision Time (GDT) a 

"Scripted Freeze" shall occur to allow time for concurrence of accomplished events. A "Resume" shall be 

required for continuation of the DOP; however a "Scripted 

Freeze" shall not occur if it will interrupt operation 

in the ATS Hold Mode. 

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5.2.7.2 SCC Initiates DOP 

1) SCC operator activates "RESUME" and monitors 

Vehicle Time on SCC CRT. 

5.2.7.3 Crewman Sets Event Timer 

1) Timer Power Switch to "Display and Aural" 

2) Timer Mode Switch to "IT Set" 

3) Insert Time "12680" 

4) Timer Mode Switch to "DT Set" 

5) Insert Time "00120" 

6) Timer Mode Switch to "Operate" 

7) Observe Timer Counting Down 

5.2.7.4 Crewman Prepares For Prepass Briefing 

1) VDP Power Switch to "ON" 

2) Press "Lamp Test" and observe"Wrong Module" 

Light 

3) VDP Power Switch to "Command" 

4) Await start of Auto-Prepass (112500) 

5.2.7.5 Crewman Performs Auto-Prepass Briefing 

1) Observe Cue, Alpha-numerics and Target No. 

1 Al P X 5 5 011 

2) Adjust Cue "Focus" and "Brightness" 

3) Adjust Alphanumeric "Brightness" 

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5.2.7.5 Continued 

4) Press "Reject" on Magnification Controller 

5) Observe Cue, Alphanumerics and Target No. 

1 A 3 A X 3 7 012 

6) Press "Reject" on Magnification Controller (Repeat 

Steps 5-6 until Prepass complete or terminated 

by computer.) 

7) Listen for Timer Alarm(10 Sec before (112670) 

end of Prepass and again at the end of Prepass 

dnd verify Timer has reached zero and is now 

counting up for Duration Time (DT). 

5.2.7.5.1 The preceding operations have demonstrated 

requirements 4.9 (Event Timer) and 4.48 

(Cue Subsystem Prepass Mode) 

AFSO. 

5.2.7.6 Crewman Prepares for Payload Pass 

1) VDP Power Switch to "ON" 

2) Set "Frame Select" to 07500 (Panel Checklist) 

3) Press "Insert and verify panel checklist displayed 

4) Setup Panels 2C and 2D according to Checklist 

5) VDP Power Switch to "Command" 

6) Await start of Payload Pass. Do not wait more 

than 10 minutes. 

7) Listen for Timer Alarm (112800) 

8) Timer Power Switch to "OFF" 

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5.2.7.7 Crewman Performs Payload Pass 

5.2.7.7.1 Group 1 

1) Activate "Cue Hold" 

2) Observe Cue, Alphanumeric and Target No. 

1 A1PX55 011 

3) Observe "ATS Track" Light ON 

4) Release "Cue Hold" 

5) Observe Slide "1" in Eyepiece and at TV Monitor 

6) (SCC Operator) Activate "Freeze" and "Stick 

Freeze" 

7) Adjust Reticle Brightness 

8) Adjust Peripheral Brightness 

9) Adjust Cue Focus and Brightness 

10) Demonstrate control stick and magnification 

control by scanning the Scene and changing 

magnification in LP Range only. 

11) Adjust Alphanumeric Brightness 

12) (SCC Operator) Deactivate Stick Freeze and 

activate Resume. 

13) Observe Peripherals 

a) Primary Target Ind. on Right Side 

(4 Green Lights) 

b) Observe Countdown 

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5.2.7.7.1 Group 1 Continued 

13) Continued 

c) Dwell Light at GDT minus 9 (GDT-9) and 

(GDT-15) 

d) Decision Time Light 

14) Observe Eyepiece Blanking at GDT 

5.2.7.7.1.1 The preceding Group has demonstrated 

the following requirments: 

4.21 (Control Stick & Magnification 

Control during Freeze) 

AFSO 

4.46 (Reticle Req) 

AFDC, 

5.2.7.7.2 Group 2 

1) Activate "Cue Hold" 

2) Observe Cue, Alphanumeric and Target No. 

2 B6PX55 022 

3) Observe "ATS Track" Light ON 

4) Release "Cue Hold" 

5) Observe Slide "2" in Eyepiece and at TV 

Monitor. 

6) Observe Peripherals 

a) Primary Target Ind. on Right Side 

(4 Green Lights) 

b) Observe Countdown 

c) Dwell Light at GDT-7 

d) Decision Time Light 

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5.2.7.7.2 Continued 

6) Observe Eyepiece Blanking at GDT 

5.2.7.7.3 Group 3 

1) Observe Cue, Alphanumeric and Target No. 

3 A7PX77 031 

2) Observe "ATS Track" Light ON 

3) Observe Slide "3" in Eyepiece and 

at TV Monitor 

4) Observe Peripherals 

a) Primary Target Ind. on Right Side 

(4 Green Lights) 

b) Observe Countdown 

c) Dwell Time Light 

d) Decision Time Light 

5) Set ATS Trackpath Select to Trackpath 1 

6) Observe Eyepiece Blanking at GDT 

5.2.7.7.3.1 The preceding Groups (1, 2, 3) 

have demonstrated the following 

requirements: 

4.20 (Scene Streaming) 

AFSO 

4.42 (Acquisition Peripheral 

Display) 

AFSO 

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5.2.7.7.3.1 Continued 

4.48 (Cue SubsystemAuto During-Pass 

and Cue Hold) 

AFSO 

5.2.7.7.4 Group 4 

1) Observe "ATS Track" Light ON 

2) Observe Slide "4" in Eyepiece and at 

TV Monitor 

3) Change Magnification between 15.88X and 

31.76X and observe Magnification change 

in both the Scene and the Reticle. 

4) Change Magnification Stick from 31.76X 

to 63.5X and observe Blanking and Slide 

Change. (Slide No. Changes color) 

5) Change Magnification between 63.5X and 

127X and observe Magnification change 

in both the Scene and the Reticle. 

6) Return Mag Stick to 15.88X 

7) Observe Eyepiece Blanking at GDT and 

"ATS Track" Light OFF 

5.2.7.7.5 Group 5 

1) Observe "ATS Track" Light ON 

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5.2.7.7.5 Continued 

2) Observe Slide "5" in Eyepiece and at 

TV Monitor 

3) Change Magnification between 15.88X and 

31.76X and observe Magnification change 

in both the Scene and the Reticle. 

4) Change Magnification Stick from 31.76X 

to 63.5X and observe Blanking and Slide 

change.(Slide no. changes color) 

5) Change Magnification between 63.5X and 

127X and observe Magnification change 

in both the Scene and the Reticle. 

6) Return Mag Stick to 15.88X 

7) Observe Eyepiece Blanking at GDT and 

"ATS Track" Light OFF. 

5.2.7.7.6 Group 6 

1) Observe "ATS Track" Light ON 

2) Observe Slide "6" in Eyepiece and at 

TV Monitor 

3) Change Magnification between 15.88X and 

31.76X and observe Magnification change 

in both the Scene and the Reticle. 

4) Change Magnification Stick from 31.76X 

to 63.5X and observe Blanking and Slide 

change. 

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5.2.7.7.6 Continued 

5) Change Magnification between 63.5X and 

127X and observe Magnification change 

in both the Scene and the Reticle. 

6) Return Mag Stick to 15.88X 

7) Observe Eyepiece Blanking at GDT and 

"ATS Track" Light OFF. 

5.2.7.7.6.1 The preceding Groups (4, 5, 6) 

have demonstrated the following 

requirements: 

4.12 (Magnification and 

Real FOV) 

AFSO 

4.32 (Image Size-Continuous Zoom) 

AFSO 

4.47 (Reticle Requirement) 

AFSO 

5.2.7.7.7 Group 7 

1) Activate "ATS Hold" 

2) Observe Slide "7" in the Eyepiece 

3) Observe Tracking at approximately 0° Roll 

4) Observe Effects of Anamorph Drive to 

Simulate Image Aspect in Pitch 

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5.2.7.7.7 Continued 

5) Observe Tracking Past GDT 

6) Remain in the ATS Hold Mode until target is automatically released. 

5.2.7.7.8 Group 8 

Skipped due to extended tracking of Group 7 

Target. 

5.2.7.7.9 Group 9 

1) Activate "ATS Hold" 

2) Observe Slide "9" in the Eyepiece 

3) Observe Tracking at approximately 30° Roll 

4) Observe Effects of Anamorph Drive 

5) Observe Tracking Past GDT 

6) "Reject" to Release ATS Hold 

5.2.7.7.10 Group 10 

Skipped due to extended tracking of Group 9 

Target. 

5.2.7.7.10.1 The preceding groups (7, 9) 

have demonstrated the following 

requirements: 

4.17 (Initial Target Location) 

AFSO 

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5.2.7.7.10.1 Continued 

4.18 (Dynamic Target Location) 

AF SO 

5.2.7.7.11 Group 11 

1) Observe Slide "11" in Eyepiece 

2) Observe Addition of Haze approximately (25%) 

for fixed total brightness and effect on Slide 

Contrast 

5.2.7.7.12 Group 12 

1) Observe Slide "12" in Eyepiece 

2) Observe Change of Haze Level approximately (50%) 

for fixed total brightness and effect on 

Slide Contrast. 

5.2.7.7.13 Group 13 

1) Observe Slide "13" in Eyepiece 

2) Observe Change of Haze Level approximately (75%) 

for fixed total brightness and effect on Slide 

Contrast. 

5.2.7.7.14 Group 14 

1) Observe Slide "14" in Eyepiece 

2) Observe Change of Haze Level approximately (100%) 

for fixed total brightness and effect on Slide ' 

Contrast. 

5.2.7.7.14.1 The preceding Groups (11 thru 14) have 

demonstrated the following requirements: 

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5.2.7.7.14.1 Continued 

4.44 (Haze Variation) 

AFSO 

4.45 (Haze Combined with Scene) 

AFSO 

5.2.7.7.15 Group 15 

1) Observe Slide "15" in Eyepiece 

2) Observe Scene Brightness Approximately (25%) 

5.2.7.7.16 Group 16 

1) Observe Slide "16" in Eyepiece 

2) Observe Scene Brightness approximately (50%) 

5.2.7.7.17 Group 17 

1) Observe Slide "17" in Eyepiece 

2) Observe Scene Brightness approximately (75%) 

5.2.7.7.18 Group 18 

1) Observe Slide "18" in Eyepiece 

2) Observe Scene Brightness approximately (100%) 

Variation 

5.2.7.7.18.1 The preceding Groups (15 thru 

18) have demonstrated the 

following requirement: 

4.16 (Lighting) 

AFSO 

4.30 (Image Intensity 

APS() 

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5.2.7.7.19 Group 19 

1) Observe Resolution Slide in Eyepiece 

2) Observe Cue Alphanumeric and Target No. 

19 A7PX55 191 

3) Observe "ATS Track" Light ON 

4) A Scripted Freeze will occur at (113132). 

The SCC operator will activate Stick Freeze. 

5) Using the Control Stick move the Image in 

both axes and observe + 4 inch motion 

in each axis. 

*6) Center the Reticle on the On Axis Resolution Target. Record the Resolution 

readings from three qualified observers 

on the attached Data Sheets, setting the 

Magnification Control Stick as indicated 

on the Data Sheets. 

*7) Remove the HPA High Power Arm and insert 

the Low Power Arm. Repeat readings as 

specified on the Data Sheets. 

*8) Activate Resume (SCC Operator). 

*9) Activate "Crippen Switch". 

*10) A Scripted Freeze will occur at (113135). 

*11) Repeat Steps 6 and 7 for LPA. 

* The number of Resolution Readings shall 

be that required to satisfy the AF 

Demonstration Team that the Verification 

Data taken for 4.33 of this Procedure is 

valid when Scene Drifts are nulled by 

the Computer. 

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Page 148 

5.2.7.7.19 Continued 

12) Activate Resume (SCC Operator). 

13) Change Manual Filter Wheel setting and 

observe Scene Brightness variation. 

14) Observe Eyepiede blanking at GDT. 

5.2.7.7.19.1 The preceding Group (19) has 

demonstrated the following 

requirements: 

4.31 (Manual Filter) 

AFSO 

4.33 (Resolution) 

AFSO 

4.36 (Optical Center Selection) 

AFSO 

4.19 (Scan Area) 

AFSO 

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5.2.7.7.20 Group 20 

The remaining Groups will be used to 

5.2.7.7.21 Group 21 

exercise normal ATS operation as follows: 

5.2.7.7.22 Group 22 1) Observe Cue, Alphanumeric 

5.2.7.7.23 Group 23 and Target No. 

2) Observe "ATS Track" Light 

5.2.7.7.24 Group 24 ON 

5.2.7.7.25 Group 25 3) Observe Peripherals 

4) Center Target and Vote 

5.2.7.7.26 Group 26 

5.2.7.7.26.1 The preceding Groups(1 thru 26) have 

demonstrated the ATS Only DOP, and 

the following requirements: 

4.2 (SLM Controls and Displays) 

AFSO 

4.7 (Operational Scripting Capability) 

4.15 (Scene Dynamics) 

5.2.7.7.27 At the conclusion of this DOP, the same Orbital 

Pass will be setup and rerun in accordance with 

Paragraph 4.6 of the Procedure. 

5.2.7.7.27.1 Completion of 5.2.7.7.27 will have 

demonstrated the following requirement: 

4.6 (10 Min Turnaround and Restacking) 

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Page 150 

5.2.8 Display Tables 

The proceding procedure defined a high density ATS only 

DOP. The following tables define for each group what 

would be observed if a vote were registered for each 

Target for both a high and medium density target pass. 

These tables allow prediction of what would be observed 

if a script were run without following a step by step 

procedure of a prescribed DOP. 

A table for a low density target pass is not shown 

since it would be an abreviated version of either a 

high or medium density target pass. 

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Page 151 

Group 

5.2.8.1 High Density Pass 

Target Cue No. Intersect # 

Primary 

Target 

Alpha - 

Numeric 

Target 

ID 

Peripheral 

Dwell Vote 

1 1 1 55 * A1PX55 011 GDT-15 I 

2 1 37 B3AX37 012 GDT- 9 I 

3 1 33 C4AX33 - 013 GDT R 

2 1 2 33 A2AX33 021 GDT- 7 I 

2 2 55 * B6PX55 022 GDT R 

3 1 - 3 77 * A7PX77 031 GDT-12 I 

2 3 55 B1AX55 032 GDT A 

4 1 4 55 A3AX55 041 GDT- 8 A 

2 4 73 * B4PX73 042 GDT A 

5 1 5 55 1 A2AX55 051 GDT- 9 R 

2 5 33 * B6PX33 052 GDT R 

6 1 6 73 A7AX73 061 GDT-10 

2 6 55 B5PX55 062 GDT 0 

7 1 7 55 * A5PX55 071 GDT-15 I 

2 7 37 B3AX37 072 GDT- 8 I 

3 7 33 C2AX33 073 GDT R 

8 1 8 33 A7PX33 081 GDT-10 A 

2 8 37 B1M37 082 GDT 

9 1 9 55 A2PX55 091 GDT- 6 

2 9 77 B5AX77 092 GDT 

10 1 10 33 * A3PX33 101 GDT-13 R 

2 10 73 B4AX73 102 GDT- 7 A 

3 10 77 C4AX77 103 GDT I 

11 1 11 77 A5AX77 111 GDT- 6 

2 11 55 B2PX55 112 GDT 0 

12 1 12 55 A1PX55 121 GDT- 7 

2 12 37 B6AX37 122 GDT 

13 1 13 77 A7PX77 131 GDT-10 A 

2 13 55 B7AX55 132 GDT 

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Page 152 

Croup 

5.2.8.1 

Target 

High Density Pass 

Cue No. Intersect # 

(Continued) 

Primary 

Target 

Alpha - 

Numeric 

Target 

ID 

Peripheral 

Dwell Vote 

14 1 14 77 A3AX77 141 GDT-12 R 

2 14 73 * B4PX73 142 GDT A 

15 1 15 55 * A4PX55 151 CDT-11 I 

2 15 33 B1A133 152 GDT I 

16 1 16 37 A3AX37 161 GDT- 7 I 

2 16 55 * B1PX55 162 CDT R 

17 1 17 33 A5A133 171 GDT-12 R 

2 17 37 * B2PX37 172 GDT I 

18 1 18 55 * A4PX55 181 GDT-12 I 

2 18 37 B6AX37 182 GDT I 

19 1 19 55 * A7AX55 191 CDT-15 I 

2 19 37 B2AX37 192 CDT- 8 I 

3 19 33 C1AY33 193 GDT I 

20 1 20 33 * A2PX33 201 GDT-12 A 

2 20 55 B3AX55 202 CDT I 

21 1 21 77 A1AX77 211 CDT-10 

2 21 73 B1PX73 212 CDT 

22 1 22 55 * A4PX55 221 CDT-15 R 

2 22 33 B5AX33 222 CDT- 8 I 

3 22 37 C7AX37 223 CDT I 

23 1 23 37 A6PX37 231 CDT-11 

2 23 55 B3A155 232 CDT A 

24 1 24 55 A3PX55 241 CDT- 9 

2 24 33 B2AX33 242 CDT 

25 1 25 77 * A4PX77 251 CDT-15 I 

2 25 73 B6AX73 252 CDT- 8 I 

3 25 37 C7AX37 253 CDT A 

26 1 26 37 A1AX37 261 CDT- 9 

2 26 55 B5PX55 262 CDT 

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5.2.8.2 

GROUP 

MEDIUM DENSITY PASS 

TARGET CUE NO. INTERSECT # 

PRIMARY 

TARGET 

ALPHANUMERIC 

TARGET 

ID 

PERIPHERAL 

DWELL VOTE 

1 1 1 55 * A1PX55 011 GDT-9 I 

2 1 37 B3AX37 012 GDT I 

2 1 2 33 * A2PX33 021 GDT R 

3 1 3 77 * A7PX77 031 CDT - 10 I 

2 3 55 BIAX55 032 GDT R 

4 1 4 55 * A3PX55 041 GDT A 

5 1 5 55 * A4PX55 051 GDT I 

6 1 6 73 A7AX73 061 GDT-6 I 

2 6 55 * B5PX55 062 GDT R 

7 1 7 55 * A5PX55 071 GDT-9 I 

2 7 37 B3AX37 072 CDT I 

8 1 8 33 * A7PX33 081 GDT-6 R 

2 8 37 B1AX37 082 GDT 0 

9 1 9 55 * A2 PX55 091 GDT I 

10 1 10 33 * A3PX33 101 GDT - 8 A 

2 10 73 B4AX73 102 CDT A 

11 1 11 77 * A5PX77 111 GDT A 

12 1 12 55 * A1PX55 121 GDT I 

13 1 13 77 * A7PX77 131 GDT I 

14 1 14 77 * A3PX77 141 GDT R 

15 1 15 55 * A4PX55 151 GDT I 

16 1 16 37 * A3PX37 161 GDT A 

17 1 17 33 * A5PX33 171 GDT I 

18 1 18 55 * A4PX55 181 GDT-7 R 

2 18 37 B6AX37 182 GDT I 

19 1 19 55 * A7PX55 191 GDT-9 I 

2 19 37 B2AX37 192 GDT R 

20 1 20 33 A2PX33 201 GDT-9 A 

2 20 55 B3AX55 202 GDT A 

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Page 154 

5.2.8.2 MEDIUM DENSITY PASS (continued) 

PRIMARY ALPHA- TARGET PERIPHERAL 

GROUP TARGET CUE NO. INTERSECT # TARGET NUMERIC ID DWELL VOTE 

21 1 21 77 A1AX77 211 GDT-7 I 

2 21 73 * B1PX73 212 GDT I 

22 1 22 55 * A4PX55 221 GDT-11 R 

2 22 33 B5AX33 222 GDT A 

23 1 23 37 * A6PX37 231 GDT-6 I 

2 23 55 B3AX55 232 GDT I 

24 1 24 55 * A3PX55 241 GDT-6 A 

2 24 33 B2AX33 242 GDT I 

25 1 25 55 * A4PX55 251 GDT-10 I 

2 25 77 B6AX77 252 GDT 0 

26 1 26 37 A1AX37 261 GDT-7 I 

2 26 55 * B5PX55 262 GDT A 

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Page 155 

5.3 MO Only DOP 

5.3.1 General 

The Test Procedure for this DOP contains the tasks required 

to verify specific requirements of the Phase 0 MDS as defined in Section 4.0 of this Document. 

5.3.2 Requirements Demonstrated 

The following requirements will be demonstrated during the 

MO Only DOP. 

Target 1 4.10 Image Velocity Sensor 

2 4.24 VO Peripheral Display 

Target 3 1 4.21 Control Stick and Mag Control During Freeze 

Target 4 

5 

4.26 Scene Lighting 

6 

Target 8 4.11 Stick Input 

thru 4.17 Initial Target Location 

Target 2 4.18 Dynamic Target Location 

4.27 Target Location Relative to Vehicle • 

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Page 156 

Target 1 - 4.2 Controls and Displays 

26 

4.7 Operational Scripting Capability 

4.15 Scene Dynamics 

4.6 30 Min. Trunaround 

5.3.3 Scripting 

This DOP contains 26 Targets for tracking in the Primary Optics. 

5.3.4 Stimulus 

The stimulus material for this DOP consists of 26 sequentially 

numbered slides. Each slide contains a grid of indexed 

intersections spaced on one inch centers across the format. 

5.3.5 Setup 

The MDS will be in an operational configuration as defined in 

the Pre-test Checkout Program BIN: BIF-055-46753-69 with all 

simulation software and AVE programs loaded. The simulated 

command messages, stimulus data and "Script" data will be 

read into the Computer Subsystem. The slides will be loaded 

into the LP arm of the SVS. 

The panel setup in the SLM will be as follows: 

1. Magnification Controller at upper limit of HP range. 

2. Control Stick centered 

3. "Crippen Switch" On 

5.3.6 DOP Procedure 

5.3.6.1 General 

This DOP will commence when the "Resume command is 

initiated at the SCC. At this point, vehicle time 

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5.3.6.1 General (Continued) 

will be 112800 seconds. 

The MDS will be operating continuously through 

the end of the Payload Pass unless the "Freeze" 

is initiated, the MDS is placed in a "Hold" configuration until the "Resume" is once more initiated. 

Then the MDS resumes operation from the point in 

time at which the "Freeze" occurred. 

5.3.6.2 SCC Initiates DOP 

1) SCC Operator presses "Resume" and monitors 

Vehicle Time on SCC CRT (112800) 

5.3.6.3 Crewman Performs Payload Pass 

5.3.6.3.1 Target 1 

1) Activate "Crippen Switch" 

2) Select "125X" on Mag. Controller 

3) Observe "MO Track" Light ON 

4) Observe Peripherals 

a) 7 Photos scheduled 

b) Wipeout countdown 

5) Observe IVS Rate Nulling 

6) Observe Eyepiece blanked at end 

of last Photo 

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5.3.6.3.2 Target 2 

1) Set Mag Controller to "MCSA" detent 

2) Observe "MO Track" Light On 

3) Observe Peripherals 

a) 6 Photos- scheduled 

b) Wipeout countdown 

4) Observe Image Rate 

5) Set Mag. Controller to "HP Range) 

6) Observe IVS Rate nulling 

7) Observe Eyepiece blanked at end of 

last Photo 

5.3.6.3.2.1 The preceeding targets (1, 2) 

have demonstrated the following 

requirements. 

4.10 (Image Velocity Sensor) 

AFSO 

4.24 (VO Peripheral Display) 

AFSO 

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5.3.6.3.3 Target 3 

1) Observe "MO Track" Light On 

2) Observe IVS Rate Nulling 

3) Activate Freeze (SCC Operator) & Stick Freeze 

4) Activate Mag. Controller to following 

positions and observe Step Magnification 

Change. 

125X 

Deactivate Stick Freeze & Freeze 

5) Activate Resume (SCC Operator) 

5.3.6.3.3.1 The preceeding target has demonstrated the following requirements 

4.21 (Control Stick and Mag 

Control During Freeze) 

AFSO 

4.22 (Magnification & Real FOV) 

AFSO 

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5.3.6.3.4 Target 4 

1) Observe Scene Brightness Approximately (25%) 

5.3.6.3.5 Target 5 

1) Observe Scene Brightness Approximately (50%) 

5.3.6.3.6 Target 6 

1) Observe Scene Brightness Approximately (75%) 

5.3.6.3.7 Target 7 

1) Observe Scene Brightness Approximately (100%) 

5.3.6.3.6.1 The Preceeding targets (4, 5, 6, 

7) have demonstrated the following 

requirement: 

4.26 (Scene Lighting) 

AFSO 

5.3.6.3.8 Target 8 

1) Mag control to "MCSA" detent 

2) Control stick to center 

3) Observe "MO TRACK" light on 

4) View target and null rates manually 

5) Exposure adjust to "INCREASE" 

6) Press "X" Format IMC "INHIBIT" 

7) Observe blanking at end of photo sequence 

5.3.6.3.9 Target 9 

1) Control stick to center 

2) Observe 1M0 TRACK" light on 

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3) View Target and null rates manually 

4) Override photo sequence by placing 

camera Select to SECONDARY and Shutter 

Mode to MANUAL 

5) Press MANUAL SHUTTER 

6) Reset Camera Select to "COMMAND" 

7) Reset Shutter Mode to "COMMAND" 

8) Observe blanking at end of photo sequence. 

5.3.6.3.10 Target 10 

1) Control stick to center 

2) Observe "MO TRACK" light on 

3) View target and null rates manually 

4) Override photo sequence by placing 

Camera Select to SECONDARY and Shutter 

Mode to MANUAL 

5) Press MANUAL SHUTTER 

6) Reset Camera Select to "COMMAND" 

7) Reset Shutter Mode to "COMMAND" 

8) Observe blanking at end of photo sequence. 

......., 

5.3.6.3.11 Target 11 

5.3.6.3.12 Target 12 

5.3.6.3.13 Target 13 

.... 

5.3.6.3.14 Target 14 

5.3.6.3.15 Target 15 

5.3.6.3.16 Target 16 

The remaining targets 

will be used to perform 

normal MO Operations 

such as manual rate nulling 

as follows: 

1) Mag Control in "MCSA" detent 

2) Control stick to center 

3) Observe "MO Track" Light On 

4) View target and null rates 

manually 

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5.3.6.3.17 Target 17) 

5.3.6.3.18 Target 18 

5.3.6.3.19 Target 19 

5.3.6.3.20 Target 20 

5.3.6.3.21 Target 21 

5.3.6.3.22 Target 22 

5.3.6.3.23 Target 23 

5.3.6.3.24 Target 24 

5.3.6.3.25 Target 25 

5.3.6.3.26 Target 26/ 

The remaining targets will be 

used to perform normal MO Operations such as manual rate nulling 

as follows: 

1) Mag. Control in "MCSA" detent 

2) Control Stick to center 

3) Observe "MO Task" Light On 

4) View target and null rates 

manually. 

5.3.6.3.26.1 The preceeding targets (8 thru26) 

have demonstrated the following 

requirements: 

4.11 (Stick Input) 

AFSO 

4.17 (Initial target Location) 

AFSO 

4.18 (Dynamic target Location 

AFSO 

4.27 (Target location relative to 

Vehicle) 

-AFSO 

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5.3.6.3.26.2 The preceeding targets (1 thru 

26) have demonstrated the MO 

Only DOP. And the following 

Requirements 

MO only DOP 

5.3.6.3.27 

AFSO 

4.2 (SLM Controls) 

(and displays) 

AFSO 

4.7 (Operational) 

(Scripting ) 

(Capability ) 

AFSO 

4.15 (Scene Dynamics) 

AFSO 

At the Conclusion of this DOP 

the ATS/MODOP will be SETUP 

in accordance with Paragraph 

4.6.5.7 thru 4.6.5.9 of the 

Procedure and Run in accordance 

with Paragraph 5.4 of this 

Procedure. 

5.3.6.3.27.1 Completion of 5.3.6.3.27 will 

have demonstrated the following 

Requirement 

4.6(30 Min Turnaround) 

AFSO 

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Page 164 

5.4 ATS/MO DOP 

5.4.1 General 

The Test Procedure for this DOP contais the tasks required to 

verify specific requirements of the Phase 0 MDS as defined in 

Section 4.0 of this Document. 

5.4.2 Requirements Demonstrated 

The following requirements will be demonstrated by this DOP: 

4.14 Target Loading and Coordination 

5.4.3 Scripting 

This DOP contains 26 groups of targets scripted for ATS Trackpath No. 1 and provides the capability to perform either ATS 

or MO tasks. 

5.4.4 Stimulus 

The stimulus material for this DOP will be three sets of slides 

(LP, HP and MO) numbered sequentially from 1 to 26. Each slide 

will contain a grid of indexed intersections spaced on one inch 

centers across the format. 

The cues for this DOP will be numbered 1 to 2.6 to correspond with 

group number. For mare than one target in a group, duplicate cue 

slides will be used. Each cue slide will contain the indexed intersection to be used as that target. 

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5.4.5 Setup 

The MDS will be in an operational configuration with all simulation software and AVE programs loaded, the simulated command 

messages, stimulus data and "Script" data will be read into the 

Computer Subsystem. 

The LP and HP slides will be loaded into the HP arm of the SVS and 

will be restacked to place LP slides in the Supply Elevator and 

the HP slides in the Takeup Elevator. The MO slides will be 

loaded into the Supply Elevator of the LP arm of the SVS. 

The SLM setup will consist of a panel checklist for Panels 2C 

and 2D. For this DOP, the controls of interest and the positions 

selected are: 

Trackpath Select to "Trackpath No. 1" 

Magnification Controller to "LP Range" 

VDP to "Command" 

Right Hand Control Stick Centered 

Camera Select to "Primary" 

Shutter Mode to "Command" 

Crippen Switch to "OFF" 

5.4.6 DOP Procedure 

5.4.6.1 General 

This DOP will commence when the "Resume" command 

is initiated at the SCC. 

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5.4.6.1 General (Continued) 

At this point, vehicle time will be 112800 seconds. 

The NDS will be operating continuously through the 

end of the Payload Pass unless the "Freeze" interrupt 

is initiated. Then the NDS is placed in a "hold" configuration until the "Resume" is once more initiated 

and the MDS continues operation from the Point at which 

the "Freeze" is occurred. 

5.4.6.2 Crewman Setup of Panels 2C & 2D 

1) Trackpath Select to "Trackpath No. 1" 

2) Magnification Controller to "LP Range" 

3) VDP to "Command" 

4) Right Hand Control Stick "Centered" 

5) "Crippen" Switch to "OFF" 

5.4.6.3 SCC Initiates DOP 

1) (SCC Operator) activates "Resume" and monitors 

Vechicle Time (112800) at the CRT. 

5.4.6.4 Crewman Performs Payload Pass 

5.4.6.4.1 Group 1 

1) Observe Cue, Alpahnumeric & Target No. 

1 A1PX55 011 

(55) 

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Page 167 

5.4.6.4.1 Continued 

2) Observe "ATS Track" Light On 

3) Observe Slide "1" in Eyepiece + Centered 

on intersection (55) 

4) Observe ATS Peripherals 

5) Vote Inactive 

6) Observe Cue, Alpahnumeric & Target No. 

1 B3AX37 012 

(37) 

7) Observe "ATS Track" Light On 

8) Slide "1" in Eyepiece + Centered on 

intersection (37) 

9) Observe Peripherals a) No Dominoes 

b) First dwell Light 

extinguished 

10) Vote Active 

11) Observe Eyepiece Blanking at GDT 

5.4.6.4.2 Group 2 

1) Observe Cue, Alphanumeric & Target No. 

2 A2PX33 021 

(33) 

2) Observe "ATSTrack" Light On 

3) Observe Slide "2" in Eyepiece + Centered 

on intersection (33) 

4) Observe Peripherals 

5) Vote Inactive 

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Page 168 

5.4.6.4.3 Group 3 

1) Observe Cue, Alphanumeric & Target No. 

3 A7PX74 031 

(74) 

Observe "ATS Track" Light On 

3) Observe Slide "3" in Eyepiece + Centered 

on intersection (74) 

4) Observe Peripherals 

5) Vote Inactive 

6) Observe Cue, Alphanumeric & Target No. 

3 B1AX53 032 

(53) 

7) Observe "ATS Track" Light On 

8) Observe Slide "3" in Eyepiece and Centered 

on intersection (53) 

9) Observe Peripherals 

10) Vote Override 

11) Set Magnification Controller to "MCSA" 

Detent 

12) Observe "MO Track" Light On 

13) Observe MO Peripherals 

14) Observe Slide "3" in Eyepiece (intersection (53) will be centered in FOV) 

15) Observe Eyepiece Blanking at end of 

Photo Sequence 

16) Set Magnification Controller to "LP Range" 

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Page 169 

5.4.6.4.4 Group 4 

1) Not viewed due to MO Tracking 

5.4.6.4.5 Group 5 

1) Observe Cue, Alphanumeric & Target No. 

5 A41AX46 051 

(46) 

2) Observe "ATS Track" Light On 

3) Observe Slide "5" in Eyepiece + Centered on 

intersection (46) 

4) Set Magnification Controller to "HP Range" 

5) Observe Eyepiece Blank during Slide 

Change 

6) Observe Slide "5" in Eyepiece + Centered 

on intersection (46) 

7) Observe Peripherals 

8) Vote Inactive 

9) Set Magnification Controller to "MCSA" 

Detent 

10) Observe "MO Track" Light On 

11) Observe MO Peripherals 

12) Observe Slide "5" in Eyepiece + Centered 

on intersection (46) 

DORIAN 

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Page 170 

5.4.6.4.5 Continued 

13) Observe Eyepiece Blanking at end of 

Photo Sequence 

14) Set Magnification Controller to "LP 

Range" 

5.4.6.4.6 Group 6 

Not viewed due to MO Tracking 

5.4.6.4.7 

5.4.6.4.8 

The remainder of this DOP will be conducted 

in this manner for the odd-numbered Groups. 

The only variation to be included will be the 

insertion of target position errors on several 

targets. The effect of these inputs will be 

observed in the Eyepiece and will result in 

the cued intersection being offset from center. 

The crewman task is to return the target to 

center prior to voting. 

Completion of this DOP will have demonstrated 

requirements. 

ATS/MO DOP 

AFSO 

4.2(SLM Controls and) 

(Displays 

AFSO 

4.7(Operational Script-) 

(ing Capability AFSO 

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...•■■., Page 171 

5.4.6.4.8 Continued 

4.14(Target Loading ) 

(and Coordination) 

4.25(Target Coordin- ) 

(ation and Loading) 

4.42(Acquistion Peri-) 

(pheral Display ) 

.I....... 

-SECRETIDORIAN 

HANDLE VIA BYEMAN SYSTEM ONLY 

.,, 

AFSO 

AFSO 

AFSO