lAW OFFICES OF WAYNE A. JOHNSON 

WAYNE A. JOHNSON, ATTORNEY 

2901 W. PARKER ROAD#864434 

PLANO,TEXAS75086 

214.454.3292 

March 11, 2016 

Docket Management Facility 

U.S. Department of Transportation 

1200 New Jersey Ave. 

SE West Building Ground Floor Room W12-140 

Washington, DC 20590 

Re: Drone Pilot, LLC 

Exemption No. 13801 

Regulatory Docket No. FAA-2015-2553 

Dear Sir or Madam: 

- ' ' 

:..-' .; 

\ .... • j ._ • !,.(! \; ~-j; 1 j 

The FAA granted the request for exemption for Drone Pilot, LLC by letter ofDecember 1, 2015 

as referenced above. 

Drone Pilot, LLC hereby applies for an amendment to the grant to (i) include the additional 

unmanned aircraft systems identified below, and (ii) permit operations for the additional purpose 

of closed-set motion picture and television filming and production. 

The Unmanned Aircraft Systems. The unmanned aircraft systems (UAS) to be added (i) are 

lightweight rotorcrafts having a maximum takeoff weight of less than 55 pounds (including 

payload), (ii) will be operated at a speed of no more than 87 knots, (iii) all contain built-in safety 

features, and (iv) are produced by UAS industry leaders. 

Proposed operations will be conducted under controlled conditions in airspace that is limited, 

predetermined, and access controlled. Operations will be subject to strict operating parameters 

to ensure at least an equivalent level of safety to currently authorized operations using manned 

aircraft. 

Petitioner proposes that it be authorized by a grant of exemption to use any aircraft identified on 

the List of Approved Unmanned Aerial Systems under Section 333 at regulatory docket FAA2007-3330 at www.regulations.gov, when weighing less than 55 pow1ds including payload. 

Petitioner also proposes that it be authorized by grant of exemption to use the DJI Phantom 4 and 

the RP Flight Systems Vigilant Cl (not currently on the list). 

-~ ---

ljPage 

These UAS have common characteristics. Each can be operated by toggle or entirely by a touchscreen, map-based interface. This means the operator only needs to command the system where 

to go, and the system does all the flying for the operator. They can be operated in both semi and 

fully autonomous flight modes, with the operator simply clicking on a map to create a preplanned flight path for a flight. In addition, the operator can create no fly zones or maximum 

flight ranges and altitudes so the system cannot enter areas deemed unsafe or unnecessary to fly 

over. 

In addition, the UAS have built-in intelligent fault handling capabilities which allow them to 

detect a system fault while in the air and automatically fly back to its take-off location and land. 

Faults that can be detected include: loss of communication; exceeding pre-set wind thresholds; 

and low battery levels. 

All flight operations are global positioning system (GPS) controlled, making the systems easy to 

navigate. At any point if the operator is not explicitly commanding the rotorcraft system to 

move, the system automatically holds its GPS position. The flight control system employs not 

only GPS positioning but a variety of sensors including sonar, barometric pressure, temperature, 

wind speed and others to ensure stability so long as wind thresholds are not exceeded. 

All manufacturers maintain online product information portals with comprehensive 

downloadable operating and maintenance manuals, user guides, flight checklists, safety 

information and mission planning instructions. Available also are instructional product and 

training videos along with robust online blogs and product forums. 

Information and specifications for the DJI Phantom 4 can be found at 

https://store.dji.com/phantom/phantom-4, and for the RP Flight Systems Vigilant Cl, see the 

attached Appendix "A" RP Flight Systems manual. 

Standard Operating Procedures, Pre-flight checklists and Post-flight checklists were filed with 

the above-referenced application for exemption. Attached as Appendix "B" is the Motion 

Picture and Television Operations ManuaL 

There has been no change in the conditions and reasons relative to public interest and safety that 

were the basis for granting the original exemption. 

Thank you. 

Wayne A. Johnson 

21Page 

Appendix "A" 

RP FLIGHT SYSTEMS MANUAL 

31Page 

RPFLIGHT' SYSTEMS INC. 

Spectra UA 

System User Manual 
----------------------------------------------------------------------------------~ 

RPFLIGHT SYSTEMS, INC. 

Spectra Micro Air Vehicle System User 

Manual 

? RPF!ight Systems, Inc. 

P.O. Box 470 

Wimberley, 1X 78676 

Phone: (512) 847-9746 
Table of Contents 

Introduction ................................................................................... 1 

Spectra Miss ion ............................................................................ 1 

How to Use This Manual .............................................................. 1 

Spectra UA ................................................................................................ 1 

Spectra Ground Control Station ............................................................. 2 

Technical Support .................................................................................... 2 

System Description ....................................................................... 3 

System Concept of Operations .............................................................. 3 

Spectra UA ................................................................................................ 3 

Ground Control Station (GCS) ............................................................... 3 

Support Material ....................................................................................... 4 

System Operation ......................................................................... 5 

Ground Prep- GCS Power On and Software Startup ........................ 5 

Flight Prep- Spectra Power Sequence ................................................ 6 

Flight Planning- Map Waypoint Selection ......................................... 1 0 

Drag and Drop .................................................................................. 11 

FOV Projection and Coordinate Reporting .......................................... 14 

Flight Sequencing ................................................................................... 15 

Flight Sequence- Upload ................................................................. 15 

Flight Sequence- Fly ....................................................................... 15 

Flight Sequence -Loiter ................................................................... 16 

Flight Sequence -Land .................................................................... 16 

System Recharge- Spectra and GCS ............................................... 16 

Operational Use Notes .............................................................. 17 

The GCS ........................................................................... ~ ...................... 17 

Launching The UAV ............................................................................... 24 

Quick Start Checklist ................................................................. 26 

UA Flight Planning and Modes .................................................. 28 

Troubleshooting ......................................................................... 29 

Index ........................................................................................... 31 
REVISION -A 

3/25/2007 

Introduction 

T his manual presents a user with the infmmation needed to operate and 

support the Spectra Mkro Air Vehicle ~A) system. The Spectra system 

includes two (2) Spectra air vehicles, one (1) Ground Control Station (GCS), 

one (1) carrying case and assorted support equipment. 

Spectra Mission 

The Spectra UA mission is simple: AJlow a user in the field to gather intelligence and 

"look behind the hill" without putting the user or any associates into harm's way. The 

Spectra conducts autonomous coYert surveillance flight while providing a live video 

feed to the user. 

ICON KEY 

Ji6 SpectrnAiocrafi: 

Ji6 Ground Control 

Station 

2! Technical Support 

How to Use This Manual 

The "icon key" at left was shows three Icons that are used to 

indicate three different subjects in this manual. 111e first is the 

Spectra Aircraft itself, the second is the Ground Control Station 

(GCS) used to control and receive information from the 

Spectra, and the last is impmtant technical details needed for general operation and 

support. 

Spectra UA 

The Spectra UA is a 48 inch airframe, powered by Li-Po electric 

batteries and constructed out of rugged impact resistant foam, ABS 

and carbon fiber material. Embedded in the foam are the important 

electronic components, including the Tiny Guidance Engine 

autopilot as well as communication modems and video camera and 

transmitter.. Future upgraded Spectras will combine these two transmitters into a 

single digit.al link. lnfo1mation specific to the aircraft is indicated in the document by 

the airplane symbol shown here. 

1 
REVISION -A 

3/25/2007 

Spectra Ground Control Station 

:/' · The GCS hardware consists of a rugged tablet PC running Windows ~~~~··/ 

; ;;;'/1; XP in conjunction with a set of hardware attached that includes 

'~-~ ... J '\: radio receivers, additional support batteries, shaker vibration motors -~~.~-2~_;:,.~~.:-.::-=. :...->.) and video to serial stream converter hardware. This system runs the 

CCD "Glass Cockpit" control panel software that provides mapping 

and video player supp01t, as well as command and control of the Spectra UA. 

Information on the GCS is indicated in the document by the computer symbol shown 

here. 

Technical Support 

./ The technical support for the Spectra UA system includes battery 

chargers, spare parts for field repair and a rugged carrying case. 

Information on this hardware and other information is indicated by 

the document symbol shown here. 

2 
System Description 

System Concept of Operations 

The Spectra UA system is shown below. The system includes two aircraft, a ground 

control station and support equipment. 

Spectra UA 

Minlawre UAV 

Eqwpoed With~ 

,, i\irrrl'lfi fJ"fl'l<;feiv("f 

• r•.1issirm Relay Trnnscei~er 

'' C:C[) V>f!fl(l Cft!ll<!fll 

• (;;Ps l{ucurvm 

Figure 1.1SPECTRA SYSTEM 

Ruggoo {ln1egTale:t Wt111 ' 

Tiltllet PC Ti:tf)ltll PC) , -~.' ~· ·~- ... ~~~-"~ ~L •• .., .. -~ .. ~· _ .. ...,_~-· 

A variant of the Spectra UA is shown below. The Spectra is an 18 inch flying wing 

with a pusher propeller power train. Embedded in the airframe core is the Tiny 

Guidance Engine autopilot with GPS, a video camera, two Li -Po batteries, a 900 :MHz 

datalink modem, and a 2.4GHz video transmitter. Also included in the airframe are 

servo motors for fin control and a DC motor for propulsion. 

Figure 1.2SPECTRA UA 

Ground Control Station (GCS) 

The typical GCS tablet PC hardware is shown below. Other tablets are used as the 

technology for battery life and daylight display readability progress., including the 

Panasonic Toughbook. Attached to the back of the GCS is additional support 

hardware including a 900 MHz datalink modem and a 2.4GHz video receiver for 

reception of the incoming video stream. A Video to USB converter provides 

digitization of video stream for the user, and a vibrating alarm indicates to the user the 

Spectra is approaching the desired target. 
REVISION -A 

3/25/2007 

Support Material 

Figure 1. 3SPECTRA GCS HARDWARE 

The Spectra UA system also includes support equipment shown in the figure below. 

This support equipment includes but is not limited to a rugged carrying case, battery 

charger, and assorted field repair equipment (tape, propellers, etc.) 

Figure 1.4SPECTRA SUPPORT EQUIPMENT 

4 
ft!S Ground Control 

Station 

System Operation 

The following list is a summary description of operating the Spectra UA System for 

video surveillance. Detailed information on each of the steps is described in depth 

later in this section 

1. Ground Prep - GCS Power On and Software Startup 

2. Flight Prep - Spectra Power Sequence 

3. Flight PJanning - Map W aypoint Selection 

4. Flight Conduct- Flight Initialization and Action 

a. Upload- sends new set of GPS waypoints to the Spectra 

b. Fly -commands launch and fly out of the Spectra to preset waypoints 

c. Loiter- selection of the waypoint to loiter at 

d. Land -landing hierarchy 

5. Video Display and Map OverJay 

6. System Recharge 

Ground Prep- GCS Power On and Software Startup 

The GCS consists of an auxiliary communications box and the command PC. TI1e 

power sequence should be: 

? Tum PC power on with aux com box NOT connected 

? Tum power on aux com box 

? Plug USB cable from aux com box into tablet PC AFTER Windows 

has successfully booted, but BEFORE control software has been 

launched 

? \"X/hen plugged in, two familiar tones should be heard, indicating the 

video receiver and modem have been initialized. 
MAll A11i!ucl~ 

(m»llirne) 

£S Ground Control 

Station 

REVISION -A 

3/25/2007 

? Load the Glass Cockpit software 

A screenshot of the default Glass Cockpit screen is shown here: 

Figure 2.1 CCD Glass Cockpit Software Instrumentation Screen 

V.deo fe~d (r~!>l 

time) 

This screen shows some key information about the unit in flight, as well as the ground 

control station. The Battery level indicator shows the GCS battery level and should be 

monitored so that the unit does not shut down due to lack of power. 

Once the GCS is powered on, the Spectra UA may be powered on. To prevent any 

potential startup problems, it is recommended that power to the Spectra occur AFIER 

the GCS control panel has been started. 

Flight Prep -Spectra Power Sequence 

The Specb:a UA is shown in the figure below. The propeller is held on by a propeller 

saver that allows the propeller to flex upon impact, preventing it from damaging the 

hardware upon landing. Also shown are the attached side fins. Fins on both right and 

left side are needed for launch and flight stal)ility. Flight of the unit is possible without 

fins, but not recommended -unstable flight will likely result and a crash will occur. 

6 
REVISION -A 

3/25/2007 

Power on / off of the unit is achieved by connecting the power connectors (male is 

battery, female is system). 

Figure 2. 2 Spectra UA 

The Spectra UA assembly occurs in the following steps: 

1) Attach propeller (ensure clear of debris and free to rotate) 

a. A correctly installed propeller is shown here: 

2) Attach fms 

a. Fin attachment is shown here: 

3) Power and initialization 

The Spectra UA is powered by connecting the battery connector to the rest of the 

system. This is shown in the figure below. Also shown in the figure are two 

cooling flaps for the motor controller. These prevent overheating of the system. 

Similar cooling holes are located over the video transmitter.. 

7 
REVISION -A 

3/25/2007 

Figure 2.3 Spectra Power is Applied by Connecting Battery Connector (Male) to System 

(Female). 

Before connectingpower, the following conditions should exist 

? The Spectra UA should be sitting on level ground after power up, with the top of 

d1e wing facing the sky. 

? A clear view of the sky is necessary for acquisition and tracking of satellites for 

GPS navigation. Failure to provide a clear sky will result in inability to fly. 

? The GCS should be kept a minimum oft foot away from the Spectra when power 

is applied to prevent RF modem interference wid1 GPS operation and dan1age to 

the aircraft electronics. 

After connecting power, the following secpence of events will take place. This 

sequence of events can take as long as 15 seconds if the GPS unit has lost 

settings and must be re-initialized 

? The Spectra UA will make an audible sound indicating the flight motor is ready. 

The GCS station will display "TGE BOOTING" in the lower status message bar. 

? TI1e Spectra UA will move the right control surface to indicate autopilot 

initialization is going to take place. It is CRITICAL that after this initial servo 

wiggles the unit remain motionless until the next step. IfVoice Notification 

is enabled, the system will announce to the user to hold the system steady. 

? The Spectm UA will move the left servo indicating that the unit initialization is 

complete and GPS acquisition has begun. This typically takes less than 1/2 second 

from d1e first elevon movement. TI1e GCS station will display ''RUNNING" in 

the lower status message bar. On the l'vfAP and GPS pages, the mode displayed 

will indicate "INIT". 

• 
REVISION -A 

3/25/2007 

o If no messages are received and the control surfaces do not move 

within 15 to 20 seconds, it is likely that there is a communication 

failure in the uplink to the plane. Power down the plane, and attempt 

again. If unsuccessful, power down the plane and system and repeat 

the ground station initialization (close the Glass Cockpit software, 

unplug the aux com box, wait until audible disconnect is heard, repeat 

plug in / startup of com box and Glass Cockpit software). 

? Between 10 seconds and 1 minute after this message, the mode indicator will 

transition to ''LAUNCH READY", indicating that there are sufficient satellites 

for a solution fix. 

o This time is directly driven by GPS satellite visibility. The GPS tab 

shows progress and satellite tracking. 

o IF NO POSITION IS ACQUIRED after 1 minutes, it is likely that 

there is some interference or other jamming preventing G PS 

acquisition. The system should be moved to a different location that 

has a clear view of the sky and no obstructions to allow acquisition. 

o THE UNIT WILL NOT ALLOW LAUNCH UNLESS 

THERE IS A GPS ACQUISTION AND SOLUTION! A 

minimum of 4 satellites must be in track to allow flight 

? If a video transmitter switch is included in the Spectra unit, it is 

recommended that this be in the OFF position until launch is ready. This 

will prevent possible overheat / brown out of the video transmitter due to 

lack of airflow cooling. 

... ... 

. .. ,. • 

0 

.. 

Figure 2A V"Jdeo Transmitter On I Off switch : 0 = on, I = Off 

9 
REVISION -A 

3/25/2007 

Cl Qual~t.y : o 

C2 ·~ual~t.y : 0 

Cll QualH,y : o 

C12 •::!uality : 0 

C13 Qual~ty : o 

C14 •2uality : 0 

C15 •:!ual~ty : 0 

Cll CNO : 0 

C12 CNO : 0 

C13 CNO : 0 

0.:14 CNO : 0 

0.:15 CNO : 0 

Figure 2. 5 GPS Status Screen Shows 7 Satelites in Solution of Varying Strength. Mode 

shows Spectra is ready for Launch. 

Flight Planning - Map Waypoint Selection 

While the system is acquiring satellites for GPS navigation, the GCS map set can be 

used to enter up to 8 waypoints into the system. Upload of waypoints should occur 

only after the unit has finished initializing. Shown below is the Map tab screen 

10 
Header 

information ---

Highlighted 

waypoint 

information 

Flight Plan 

commands: 

Upload 

Loiter (now) 

Land (now) 

Fly 

Abort 

Resume 

REVISION -A 

3/25/2007 

Drag and Drop 

Figure 2.6 Spectra GCS Flight Planning Map Screen 

The map screen supports drag and drop / point and click functionality. Clicking on a 

section of the map and dragging it will scroll the unit, and clicking on waypoints will 

show the defmed actions to be taken at those points. 

The function keys at the bottom of the map represent capabilities specific to the map. 

A description is shown in the figure below. 

11 
New Waypoint 

Delete 

Current 

Waypoint 

REVISION -A 

3/25/2007 

Select Map Directory and 

settings Current waypoint properties 

I 

Save 1 Zoom in J 

Load . out 

waypo1nt 

files action current 

waypoints 

I 

Figure 2. 7 Spectra Map Functions 

The map functions have the following properties: 

MAV 

Start new 

waypoint file 

? Add I Delete Waypoint- Add will place a new waypoint in the center of the 

current map screen. Delete will delete the currently highlighted waypoint. 

? Undo I Redo- Self explanatory 

? Save I Load Waypoint ftle- .wpt ftles can be created or uploaded that have 

stored waypoint ftles for the system 

? Zoom (+I-) -will zoom the map in and out within range 

? GOTO- Sets mapping functions and data paths (described later) 

? Goto ~xt Waypoint - This button will highlight and zoom to the next 

waypoint in the sequence. It is only for ease in navigating the map screen, and 

has no affect on the aircraft 

? See All W aypoints - This button will scale the map to include all current 

waypoints 

As indicated, tl1e GOTO button enables the following setup screen for map data and 

contour scaling 

12 
REVISION -A 

3/25/2007 

... 7;c:l .... , 

Go To location .. ···" • . ·,., 

rOataSource -~-

Path: I• 

Format: I CADRG 

DTED Path: IC:\code\ccdpanei\Release\ma1 ~ 

Load 

r-Loaded Map Info -------------------

CA.DRG format .... 

2221 frames inA.TOC 

Rough Latitude extents: 

N 18 deg 51.172 min· N 42 deg 3.384 min 

Rough Longitude extents: 

W 160 deg 35.465 min· W 117 deg 5.482 min 

DTED format 

167 frames loaded ..:J 

Cancel 

IDTED settings ---·---- -"-! 

I Minimum Elevation r.: 10:------::u':"'1. 

1 (Blue level): ...::.J 

! 

I Maximum Elevation 

(Red level): j6oo 

I P Color Map Based on Elevation I 

Set ____ _j 

rLocation --------··-----

I 

! Map Series: j1 :50K 

j Latitude:j ~N~33~d~e-g~3~5~.0~2--5-m-in ____ _ 

Longitude: jw 117 deg 45.715 min 

MGRS: 111SMT2929716265 

Go 

World View 

Figure 2.8 GOTO Map Adjusbnent Screen 

The GOTO Map Adjustment screen contains four frames. 1be frames contain the 

following information and actions: 

? Data Source 

o Path: Path to the CADRG data set to be used for flight operations. 

Typically, a CD of CADRG map data for a selected region will be 

loaded onto the GCS. This path indicates where t11at data is stored. 

o Fonnat: CADRG or imagery data (an advanced option if satellite 

in1agery is available) 

o DTED Patl1: Path to the DTED elevation data set to be used for 

flight operations. Typically, a CD of DTED map data for a selected 

region will be loaded onto the GCS. This path indicates where that 

data is stored. DTED Ievell is recommended. 

? Loaded Map Info 

13 
REVISION -A 

3/25/2007 

.·' 

o A summary of the loaded map data based on the paths in the ''Data 

Source" section. 

? DTED Settings 

o Used for scaling of the colors applied to the maps, the minimum 

elevation (in meters) and maximum elevation are entered here for 

visual cues to elevation if the DTED data is available. This is an 

option, and if not desired the "Color Map on Elevation" box should 

be left unchecked. 

? Location 

o TI1e current map series (CADRG defined), as well as the current view 

Latitude, Longitude and MGRS coordinates are shown. Typing new 

coordinates into this location and hitting "GO" will reset the view of 

the map screen. 

FOV Projection and Coordinate Reporting 

Shown on the map screen below are a number of important features. A description of 

each follov,-s: 

? Aircraft Information: This banner shows current aircraft position, altitude, and 

heading information. The current flight mode 0nitialization, launch, flight, 

loiter, land) is shown, as well as an ETA and distance remaining to the next 

waypoint. 

? Cursor Information: Hovering the cursor over the map provides latitude, 

longitude, altitude (if DTED data is provided or available) as well as MGRS 

coordinates. 

? Command Buttons: 'TI1ese buttons are used for deftning the commanded 

mode of the system and are described later in this document. 

? Status Messages: These messages provide the user with information regarding 

the air vehicle health and operation. 

? FOV projection: TI1is red outline indicates tl1e video camera field of view, and 

can be used to determine where tl1e aircraft video camera is currently looking. 

14 
REVISION -A 

3/25/2007 

ttd:tr~JJlL~p)~ a::wtfi-;-~~-=;-~-lb~~-:~J ~~:U;;~£-:::u-· --

Instruments! Relds ~Vide of Config jMemoryl User DBIB l Graphs I Raw[~P' GPS I 

.. -~- N "'3 deg 4<: .~s -mifl -------- sa ft 15 cteg. ' ' ' • 111 117 deg 55.305 l'l>1n 

:" , , HSHT14Se329B2o 

- No Hessages Received -~5Hz ----~-·--

:1 

Status Messages 

----~1 

FOV Projection 

Command Buttons 

Figure 2.9 FOV Projection and Coordinate Reporting 

Flight Sequencing 

I Aircraft coordinates, 

caltitude and heading, 

l

':aswell as mode, ETA 

and distance to next 

waypoint 

Cursor Lat/Long/Ait 

Height and MGRS 

! Function Keys 

The following list describes the modes of operation for the Spectra UA System 

Flight Sequence- Upload 

This button will upload the current set of 8 waypoints to the Spectra UA. The current 

set of waypoints stored in the UA will be ovetwritten with the new set. 

Flight Sequence- Fly 

This button will command the Spectra to enter flight mode. Provided a GPS lock has 

been achieved, the Spectra will begin to look for indication that the user has hand 

launched the unit. W'hen thrown with enough speed, the propeller will start to turn 

and the unit will climb to altitude. 

15 
REVISION -A 

3/25/2007 

Flight Sequence- Loiter 

Tins button will command that the current highlighted waypoint be used as the loiter 

point for the unit if desired. If no loiter point is entered, the Spectra will proceed along 

the designated waypoint path from launch to land. 

Flight Sequence- Land 

This button will force the unit to cut power and land immediately. 

System Recharge- Spectra and GCS 

The Spectra UA contains two, kell Lithium Polymer batteries with a 2100 mAhr 

capability each. The system should be charged with a L-Po charger that is set for 

charging a 3-cell, 11.1V battery set to a 4,200 mAhr capability. This would allow a 2 

amp charge capability if using a Thunder Power or equivalent charger. 

The Auxiliary Communications Box contains a single 2100 mAhr, 3-cell, 11.1 V battety. 

There is no battery indicator on the aux com box. It should be recharged after 1 hour 

of use. 

The GCS should be charged using it's AC power adapter if possible. The GCS 

contains a Li-Po battery as well, but has more capacity and could be damaged by failed 

charging capability. From depletion, a full charge may take as long as 4 hours for the 

GCSsystem. 

16 
Operational Use Notes 

TI1e actual operation of the system requires time in service to be most effective. This 

section contains notes from the development and prototype testing that should help 

other users fly the Spectra system. 

TheGCS 

The Ground Control station is a rugged tablet with USB connected communication 

devices on the back Do not disconnect the USB cables during operation, as you 

will lose communication with the UAV and potentially lose the UAV itself. 

There are six (6) main tabs of interest here. Each is described briefly below. 

COCKPIT 

The Cockpit screen shows the artificial horizon and battety voltages of interest. Pib.is 

screen is useful for determining general system health. 
!5 : 3 

REVISION -A 

3/25/2007 

F!1ght l!ode : 0 

TI>rottle : -1.0000 

VIDEO 

The video tab displays the 640 x 480 video stream in real time. This is the la1gest 

display of video in the control panel. Located on the left are the last three projected 

locations d1at are logged when the user double clicks on the video image. These 

locations are presented on the map page as flags. 

If no video is present (indicating a GCS system failure), then the display "No Vireo" 

will be shown. 

18 
REVISION -A 

312512007 

S/WSetup 

[00:22) 

This screen allows setup of RF power on the aircraft as well as local settings on the 

ground station (like communication channeQ. Besides the communication port 

number, which may change depending on port plugged into the system, none of these 

settings should be changed. They are for advanced users and experimentation 

applications. 'The following settings may be changed: 

Listen Only - If you want to use the system as a duplicate and to only view data 

coming from the UA V, click this icon. When activated, no command and control will 

occur from this unit. 

ACK - Used for the deadman switch on the UA V. For prototype testing, the 

deadman capability will make the plane return to home Qaunch point) if 

communication with the ground station is lost. 

:MISC Options- Enable Vibration Alert-This enables I disables the motor vibrator. 

:MISC Options - Voice Notification - This enables I disables audible voice 

notifications of system state. 

19 
REVISION -A 

3/25/2007 

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r.• .:r.·a·( •. -. ~-r ·"· -~-r (CO J•] 

COMMAND 

This tab provides access to a number of additional commands. Important commands 

include: 

Re·lnit Gyros -If the system was powered while being handled, or the rates shown 

indicate that the rate sensors were improperly initialized, set the unit down in a 

motionless position and dick on this item. TI1e gyros will be reset to a known zero 

value. 

Come Home - System will be commanded to return to the launch point This 

command is useful to force the unit to return to the user no matter where it is in the 

flight path. 

Throttle ++ / - : Ths allows modification of the throttle on the plane. The 

reduction(--) is particularly useful for landing the plane gradually. A COME HOl\ffi 

command will make the plane return to the user, and as it approaches multiple 

THROTTLE- commands will decrease it's altitude and allow closer landing. IT IS 

IMPORTANf 1HAT YOU «ABORT'' or «LAND ~OW'' the system before it hits 

the ground to make sure there is no damage to the system. 

20 
REVISION -A 

3/25/2007 

Center Servos On (and Oft) turns motor off and centers servos for optimum 

storage configuration. Use this before powering down the system to stow it in the 

carrying case. Tum it off if this was accidenta11y engaged and you want the unit to fly. 

IMPORTANT- Do Not Turn This On During Flight- Plane will crash!! 

Deadman Toggle enables I disables the deadman function. If enabled (default) 

and the UA does not hear from the ground station for 20 seconds, the Spectra UA will 

enter «Come Home" mode. If, after another 40 seconds, no ground communication 

bas been heard, the system will go into a ''Land Now" mode. 

Disable this function if long distance (> 1km) flights are intended or if the GCS may 

not be aJlowed to transmit an acknowledge to the aircraft. 

~ . .. . . ~~-- . 

. 

~ :o2.021 

GRAPHS 

This tab displays real-time sensor data and can be important to check caJibration. If 

the accelerometers do not record a +I -1 when oriented with the ground, the 

accelerometers should be recalibrated. If the magnetometer va1ues exceed + 1-1 then 

the magnetometers should be recaJibrated. Contact CCD for recalibration procedures. 

21 
REVISION -A 

3/25/2007 

MAPSAlready described in this manual, path planning, launch, Loiter Now, Land Now, and 

Abort/ Resume commands are active here as well as on the Command Tab. 

22 
REVISION -A 

3/25/2007 

I) 

P.laY.B c o er1 lAUNCH Command Rece~ved- . ~I001IDQJ\tli:llml : . ~ - . ,_.- - ., ' 

111is is a critical tab. It provides the user with infotmation regarding GPS lock. 

Without lock, there cannot be any flight. 

23 
REVISION -A 

3/25/2007 

C13 Qualit.y : 0 

C14 Quallty : 0 

C13 •:NO : 0 

C14 CNO : 0 

~ 

C15 Quallty : 0 C15 CNO : 0 

L,;,UIK H (_.'C,I(ilnano:l I=":.:>U'I·1'?'1 [00:06) 

--------------------~ 

Launching The UAV 

111e sequence for flight is as follows: 

? Power system on 

? Verifv attitude and healtl1 

? Upload waypoints 

? Command launch 

? 1l1row aircraft into wind, at a clear segment of sky (i.e. no trees if possible) 

1ne unit will hold the heading when launch is detected by a 4G tl1row. It is 

IMPORT ANT iliat you throw the plane level and straight. The heading is locked in at 

launch, and if ilie arm is cocked or there is oilier interference on launch, it could affect 

flight. Shown here are the suggested orientations for launch (using an older pusher 

propeller version of the Spectra UA). 

24 
REVISION -A 

3/25/2007 

Note that the wing should be pointed up at approximately 30 degrees. The unit should 

be thrown like a dart, shown here: 

Do NOT throw the unit like a baseball, cocking your wrist, as shown below. It 

will lock in a 45 degree or more offset on launch that will like cause a loss of 

altitude on launch, possibly hitting the ground. 

25 
Quick Start Checklist 

The following list should be used for simplified flight operations. 

? Turn on GCS and ensure that auxiliary hardware is powered and attached via 

USB cable(s). 

? Startup Glass Cockpit software: 

o Verify red TX indicator in bottom left corner is blinking once per 

second (datalink is active when this is true) 

o Verify "No Video" is NOT displayed on video screen (video reception 

is active when this is true) 

? Place Spectra UA on level ground Do not hold in hand, and do not allow 

wind to be moving plane for initialization. 

? Connect power wires for Spectra UA and leave undisturbed 

? Verify status messages indicate ''TGE Booting" within 5 seconds of power on 

If Voice Notification option is turned on, unit will audibly indicate booting and 

other messages. 

? \~fait for initial right elevon wiggle, then left wiggle, making sure unit is 

motionless during this time. Do not hold in hand during this time, and do not 

let wind gusts move plane. After wiggles are complete, you may move the 

plane as you would normally. Do not shade unit from acquiring satellites for 

GPS navigation. 

? Once a GPS lock is achieved, the Spectra UA will appear on the map screen. 

Verify waypoints for mission are entered correctly and choose UPLOAD on 

the map page to reprogram Spectra UA 

? Click on FLY when reported MODE on map screen indicates 'Launch 

Ready" 

o IF "GPS LOCK LOST' message appears after launch command is 

received, unit has lost lock and WILL NEED TO BE 
REVISION -A 

3/25/2007 

COMMANDED 

THROWING! 

TO LAUNCH AGAIN BEFORE 

? Throw Spectra straight and with speed and at a pitch angle of 30 degrees 

towards a clear flight path (no obstructions, etc.) 

? Spectra will fly in the direction of the lannch until 60 feet above the launch 

altitude. It will then proceed to first waypoint location and altitude. 

? Depending on path planning, Spectra will either Loiter at designated position 

or fly to each successive waypoint. If the last waypoint is reached and it is not 

designated as a LAND waypoint, the path will continue with the first 

waypoint. 

? Buzzer will sonnd and vibrate within an estimated 30 seconds of approaching 

the nextwaypoint. IT IS HIGHLY RECOMMENDED TO DISABLE 

THIS BUZZER ON THE S/W SETUP PAGE TO SAVE POWER 

ONTHEGCS. 

? View Map and Video screens to receive intelligence on activity within FOV. 

o Clicking on the video image will drop a flag on the map indicating the 

point of interest. A buffer of three (3) points of interest will be 

updated in a first in - first out manner. 

? Click on "LAND" if unit should land immediately. Click on ''LOITER" if a 

Loiter is desired at the current position. Click on ''RESUME" to break loiter. 

Click on "ABORT" to shut the motor off and glide to the ground 

immediately. 

? Last waypoint will be default to be a landing point for nnit in lieu of LAND 

command If this waypoint is turned to "CONTINUE", the UA V will fly thru 

all waypoints repetitively. 

27 
REVISION -A 

3/25/2007 

UA Flight Planning and Modes 

The Spectra UA performs the following actions in different aspects of it's flight modes: 

? INIT -No GPS lock has been achieved, flight will not be allowed. Waypoint 

planning and upload is allowed however. 

? LAUNCH READY- GPS Lock has been achieved. If a ''Launch" or "Fly" 

command is received, the unit will wait for a hard throw to proceed to the 

CUMB mode. When the hard throw is detected, the current heading is 

locked into memory before proceeding to the climb mode. If, during this 

mode, GPS is interrupted, then a "GPS Lock Lost" message will be received, 

and any "Launch" or "Fly'' command previously sent will have to be resent 

once Launch Ready mode is entered again. 

? CUMB - In this mode, the heading sensed on launch is held and the unit 

tries to achieve altitude of the first waypoint. This mode will be active until the 

following criteria are met 

o If the GPS measurement indicates that the UA is 20 meters ( -60 feet) 

above the law1eh point, then d1e unit will transition to WAYPOINTS 

mode 

o If, after 20 seconds, the UA has not achieved altitude of 20 meters, it 

will tum 180 degrees around and continue to try for altitude. 

o If, after 40 seconds, the UA has not achieved altitude of 20 meters 

above launch, the motor will shut down. It is assumed that there is 

somethingwrongwith the UA mechanics. 

o 1 second after launch, another 4 G shock to the system will tum the 

motor off as well. This is a safety feature. 

? WAYPOINTS- This is the notmal flight mode. In this mode, the buzzer 

will be active and vibrate when the ETA is less than 30 seconds. 

? LOITER- In this mode, the system is loitering about a waypoint or about a 

commanded position. 

28 
Troubleshooting 

Primary issues encountered are as follows: 

? No Red "TX" light or communication with plane 

o GCS system may not have booted properly. Follow the steps below: 

J!S Shut down all programs and power UA dov.n. 

J!S Disconnect USB cables from Tablet. Wait for audible 

indication of disconnect. 

J!S Reconnect and wait for audible indication of reconnect 

J!S Open XCTU program to see list of available serial ports 

Qooking for USB to Serial p01t in particular). 

J!S Close X -CTU program and open Glass Cockpit. 

2S On SIW setup page, make sure that the com port is the same 

as that specified by X-CTU. Also, verify that "ACK" is 

checked and ''Listen Only'' is unchecked. 

2S Hit ''RECONf\lECT'' and red ''TX" light should begin. 

? No map data is shown 

o Verify map data file is for the area where system is being used 

o Use the "GOTO" button on the map page to setup map data entries 

o Wait for GPS lock from UA, then hit the Plane button to zoom to the 

location of the actual plane. Zoom in to the correct scale for the map 

data being used. 

? Plane did not turn propeller on when I threw it 

o Launch command not sent I received - verify via status message I 

voice notification that the launch command was received. 

29 
o The GPS never achieved lock- verify lock before throw 

o The GPS lost lock after the launch command was received -tum 

audible notification on to warn of lost lock before throwing plane. 

30 
battery, 2, 5, 7, 8, 9, 18, 19 

CADRG, 15, 16 

DTED, 15, 16 

FOV, 16, 17 

GCS, 1, 2, 4, 6, 7, 10, 12, 13, 15, 18, 

19, 29, 30, 32 

Glass Cockpit, 2, 7 

GPS, 3, 6, 10, 11, 12, 17, 25, 29, 31, 

32, 33 

31 

launch, 6, 7, 16, 18, 21, 22, 24, 26, 27, 

29, 31, 33 

Spectra UA. 0, 1, 2, 3, 4, 6, 7, 9, 10, 17 

MGRS, 16 

servo, 3, 10 

Tiny Guidance Engine, 1, 3 

Waypoint, 6, 12, 14 
P.O. Box 470 Wimberley, TX 78676 Phone: 512.847.9746 

SPECTRA 

Fie I d Manu a I 

Three Camera Module 

Continued 

All Content & Images Copyright© RPF!ightSystems, Inc. 

I 

/ 
P.O. Box 470 Wimberley, TX 78676 Phone: 512.847.9746 

RPFlight Systems Spectra is shipped in its carrying case as shown below. Take the time to look over the contents before 

removing items so that you can easily return them for transp01t later. . Familiarize yourself with each of the items and 

the nomenclature used for each. The more familiar you are with each component makes this field manual easier to use. 

All components will be identified in this manual and with representative pictures of each. Some images may not look 

exactly like your platfonn, but the focus of the image will be described in the text to help clarify it's use. 

1. Ground Control Unit 7. 12V Lithium video battery 

2. Lumix DMGLX2 Digital Camera 8. Lumix Software and Manual 

3. Yellowjacket Diversity Video Receiver/Antenna 9. Lithium charger 

4. Lumix Battery Charger 10. Spectra Flying Wing 

5. 12V 4200 mah Lithium Polymer Flight Packs 11. Parts/Tool Kit 

6. Ground Contwl Charger 12. Spare Propellers 

Continued 

All Content & Images Copyright© RPFlightSystems, Inc. 

/m· /t!J, 

, c, 

" .. 
P.O. Box 470 Wimberley, TX 78676 Phone: 512.847.9746 

The one piece Spectra flying wing is a greatly simplified version of the original three piece modular design. The equipment is cradled in foam and is well protected. It is very easy to gain access to the main payload area of the Spectra, exposing the digital camera, flight pack, video pack as well as other flight electronics. 

I 

·J&:.· ...... ·._.) . : .. , I 

<-Remove the 1/4-20 nylon 

screw holding the top fairing. 

With the aircraft facing --"., ( 

towards you, carefully rotate Ill,/ 

the top to the left side of the 

aircraft as shown . 

Payload Area Components 

I. Outrunner Electric Motor 6. Camera Shutter Servo 

2. GPS Unit 7. Flight Control Receiver 

3. On Screen Display Elecb:onics (OSD) 8. Main Flight Pack Power Plug 

4. Video system power plug 9. Thermal Stabilization Switches 

5. Lumix Camera Cradle 10. Thermopile ribbon cable 

Continued 

All Content & Images Copyright© RPF!ightSystems, Inc. 
P.O. Box 470 Wimberley, TX 78676 Phone: 512.847.9746 

Adding the payload components 

The most typical requirement for your Spectra will be for the collection of high resolution digital imagery. The Lumix included with your flight kit is a very capable imager and will take excellent pictures 

from all altitudes. We have found the best results are produced by using the following settings: 

Make sure the proper aspect ratio is 

selected on the barrel of the lens. 

16:9 gives the widest angle available. 

After power up the Lumix, make sure 

the function dial on top is set to 

"SCN" or SCENE. 

I 

(:::J The screen will display several 

-1 available SCENE possibilities. 

Select the "SPORTS" mode. This gives 

the highest shutter speed possible. 

Place the camera in the cradle and 

ensure the shutter servo arm will 

contact the shutter button. 

We highly encourage the user to explore the other settings on the camera and experiment with what works best in the conditions 

most likely encountered. There are other settings that we have found effective and they are as follows: 

1. We have learned that setting the autofocus mode to MANUAL and setting the focus on infinity speeds 

up the time it takes to take a picture. 

2. Setting the Optical Image Stabilization mode to "NONE" or "OFF" actually helps to sha1pen images. 

3. If images are going to displayed on a standard TV screen set the aspect ration to 4:3. 

4. Using fast SD cards shortens the time between shots. 

5. If you are required to wait before launch, be sure to shoot one shot every 10 minutes to keep the camera 

from going into sleep mode. 

Continued 

Al1 Content & Images Copyright © RPFlightSystems, Inc. 
P.O. Box 470 Wimberley, TX 78676 Phone: 512.847.9746 

Preparing for flight operations 

WARNING! Do NOT plug in the main flight pack batteries unless the 

ground control station is turned on and tuned to the correct frequency! Doing so could place the operator and bystanders in risk 

should the motor start unexpectedly! 

~ Ensure that the ground control unit 

V is on the correct frequency for the 

aircraft you intend to fly. 

After power up of the GCU, ensure 

the correct model is displayed on the 

GCUscreen . 

. Once the GCU is powered up, connect the main flight pack as shown. 

Try to connect it smoothly without multi 

contacts of the connector. 

Place the main flight pack into the 

nose of the aircraft as shown .. 

When connected, ensure that all bystanders are clear of the propeller in 

case of radio interference . 

...,..,.---.... If the digital imager is to be used, test 

the shutter control now to ensure 

Continued 

All Content & Images Copyright© RPFiightSystems, Inc. 
P.O. Box 470 Wimberley, TX 78676 Phone: 512.847.9746 

Preparing for flight operations 

If the live video feed is to be used, 

locate and plug in the small 12V lithium polymer battery to the correct plug in 

llie aircraft. 

The video battery pack is placed behind the digital image carrier as 

T===:::======~==~~shown. 

~====~~====::!_ 

Locate the correct winglet and insert 

the pins into llie sockets, securing the 

winglet to the wing 

The winglets should fit snugly 

against the wing tip as shown 

After ensuring lliat all flight controls 

are functional, replace the pod top on 

the airframe and secure with the 1/4-200 

nylon bolt. 

After flight preparation and before 

launch, keep aircraft away from byLr::=~======~~~::::==:::J standers and support personnel. 

Continued 

All Content & Images Copyright© RPFlightSystems, Inc. 

r~' I 
Field Pre-Flight Checklist 

Print and laminate this checklist for field use before every launch! 

1. Check voltage on batteries/systems to be used 

2. Tum on, and insert imager in payload bay 

3. Plug in video battery (if used) 

4. Ensure proper frequency of ground control unit (GCU) 

5. Tum on ground control unit (GCU) 

6. Verify correct model is selected on GCU screen 

7. Announce "GCUpowerup and ready!" 

8. Plug in main flight pack and insert in airframe 

9. Announce "Airframe armed!" 

I 0. Check function of imager/payload servo 

11. Re-assemble pod top with nylon screw 

12. Verify video signal is available and transmitting (if used) 

13. Ensure on screen display (OSD) is functional 

Flight Control Check 

1. Check for correct elevon movement UP-Pull back on 

right GCU stick, elevons should move UP. 

2. Check for correct elevon movement DOWN-Push forward on right GCU stick, elevons should move DOWN 

3. Check for correct elevon movement LEFT -Move right 

stick GCU stick to the left. Left elevon should move up 

and right elevon should move down (as viewed from the 

rear) 

4. Check for correct elevon movement RIGHT -Move 

right stick GCU stick to the RIGHT. The right elevon 

should move up and left elevon should move down (as 

viewed from the rear) 

5. Announce "Stand clear of prop!'' and move the left GCU 

stick forward to ensure correct rotation of propeller. 

6. Announce "Ready to launch" and move to the planned 

takeoff zone. 

Flight Safety Procedures 

1. Review primary launch and landing site with all 

personnel before launch. 

2. Plan for the shortest possible flight time unless 

the mission calls for extended orbit of video 

feed. 

3. Designate observer(s) for each and every flight. 

4. Do not allow personnel not directly associated 

with the mission to talk to the pilot in control. 

5. Plan a contingency landing site for hazardous 

nnss1ons. 

6. In NIMS structured incidents, do not launch 

without prior approval of the Incident Commander or incident designated "airboss". 

7. Pilot should announce "Launching!" so that all 

personnel involved can hear. 

8. Pilot should announce "Landing!" so that all 

personnel involved can hear. 

9. Observer(s) should fall back to the landing site 

(if possible) and act as safety personnel to keep 

landing site clear during final approach. 

10. Pilot should announce "Aircraft secure!" and 

advise IC or incident "airboss" that the aircraft 

is down and secured. 

Continued 

All Content & Images Copyright© RPFiightSystems, Inc. 
P.O. Box 470 Wimberley, TX 78676 Phone: 512.847.9746 

Air Crew Designations-Current FAA descriptions as of August 2008 

Pilot in Command (PIC)-This person is primarily responsible for mission planning and overall operation of the mission. Pilot in Command will take into consideration any and all operating procedures as set forth by the agency requesting the mission. 

Pilot At Controls (PAC) - This individual is primarily responsible for the safe operation of the aircraft, and to execute 

the mission as set forth by the Pilot In Command). The Pilot in Command and the Pilot At Controls may be the same 

person in some circumstances. 

Observer-This position is to act as a back up and assistant to the Pilot At Controls. This person will observe the aircraft dwing its' mission and will also advise the PAC if full scale aviation assets should enter into the mission area. 

Seconda1ily, this person will act as a safety officer during takeoffs and landings. The Obse1ver MAY NOT act as both 

the Pilot At Controls and Observer concwTently dming the mission. 

Launching the Spectra flying wing 

After successful completion of the pre -flight checklist, the 

Spectra should ready to perform its' mission. The most hazardous conditions for you aircraft exist during launch and 

landing as the aircraft is close to the ground and subject to 

swirling winds and unexpected circumstances. It is advisable that the Spectra be launched by someone other than the 

Pilot At Controls (PAC) so that clear focus on flight of the 

Spectra can be maintained .. Whomever selected should have 

previous experience launching the trainer aircraft to ensme 

success. The keys to a good launch are as follows: 

1. Launch directly into the wind with as much clear space 

in the climb out area as possible. 

2. Keep the wings level as possible during launch and 

climb. 

3. DO NOT launch with power on unless medical personnel are standing by. 

4. Use 100% power to initiate climb out after the aircraft 

has left the hand of the launcher. 

5. When a good climb rate is established, reduce throttle to 

80% until mission altitude is achieved. 

6. In windy conditions, be ready to conect for extreme 

maneuvers that could be caused by ground turbulence. 

7. If a collision after launch becomes imminent, reduce 

power to zero as quickly as possible to reduce damage 

both to the aircraft and on the ground. 

Continued 

All Content & Images Copyright© RPFiightSystems, Inc. 

"1 ~-! . . •, 

+ -~~- -- . - - .• ...,,_,...., 

:~-; ~-.~..:~:--:_~~..:;.;~4" 
P.O. Box 470 Wimberley, TX 78676 Phone: 512.847.9746 

Flying the Spectra wing 

The Spectra has been designed and modified over 7 years of field trials. It is the 

best compromise between a rugged, robust airframe and a very stable aerial 

platform. The Spectra has flown and executed it's missions in environmental 

conditions that would "ground" most other small unmanned aircraft. 

1. Always pre-flight your aircraft before launch. Check that all surfaces are 

sound and that movement of the controls coincides with the appropriate 

stick on the flight control transmitter. 

2. Remember that as the aircraft flies toward you, and to correct for a bank, 

"the low wing gets the stick". For example: if the wing is flying toward 

you and from your perspective, the left wing is down, to correct for that, 

you move the stick to the left or toward the "down" wing to correct and 

level the wing. 

3. Launch sequence doesn't require as much control as you think. Just keep 

the wings level and the aircraft will find its own climb rate. If it "balloons" 

up too much and looks likely to stall, then slowly feed in a very small 

amount of down control. Throttle settings for normal operation are as follows: 

a. Launch : 100% power for the first 5-l 0 seconds or until a positive 

climb is established. 

b. Sustained climb : 75-80% power until at altitude. 

c. Cruise : 50-60% power 

d. Slow flight/endurance : 30-40% power 

e. Landing : 0% power-blip throttle as needed to control a short 

approach 

4. ALWAYS LAUNCH DIRECTLY INTO THE WIND-NEVER 

ATTEMPT A DOWNWIND LAUNCH! 

5. Landing sequence: The best landing sequence allows you to utilize a long, 

straight in approach directly into the wind. As the aircraft circles into the 

pattern, you can bleed off airspeed and altitude by pulling back very slowly 

on the elevator stick. Ifthe throttle is off, the nose should come up, and it 

should slow down significantly, and begin a gradual descent. 

6. If you fly your aircraft until it hits low voltage cutoff (L VC) you should 

begin your landing sequence immediately! This "safety circuit" keeps 

from discharging your batteries to deeply. You will know when you reach 

L VC when the throttle cuts unexpectedly. This is done to conseiVe enough 

battery energy to power the control surfaces. You should have enough battery power to make one or two short throttle bursts to control your descent. 

7. Try to flare the wing before landing to reduce forward speed as much as 

possible. Don't pull up too soon or you will stall and it will drop quickly, 

possibly damaging components. 

Continued 

All Content & Images Copyright © RPFlightSystems, Inc. 
P.O. Box 470 Wimberley, TX 78676 Phone: 512.847.9746 

Standard Video Receiver and MUX Check List. 

I 

.. . ·-

1. Video Patch cable 2. 2.4 Ghz video receiver 3. 8 dbi polarized patch anetnna 

4. LCD Monitor Patch cable 5. LCD Video Monitor 

The video system includes all the following items, plus the video TX and cameras in the Spectra. The wiring is straight forward The video RX is set to receive on channel 1, but can be 

switched to a different channel if required. Take note that the video patch cable has only two 

RCA jacks and one mini -stereo jack. The LCD monitor has 3 RCA jacks and two stereo jacks. 

Included is a gender changer for connecting two male RCA jacks. Setup of the video system 

will be as follows: 

1. Locate the video RX and insert mini stereo plug into the "AV Out" jack. 

2. Plug in a 12V power source to the RX (2.5A lead acid battery) 

3. If the antenna is not attached, screw the type "F" connector from the antenna to the RX 

4. Locate the color LCD monitor and insert the yellow mini stereo plug into the "AV In" 

5. Plug in a l2V power source to the monitor (2.5A lead acid battery) 

6. Plug the two male (yellow) RCA jacks into the gender changer 

7. Power up the LCD monitor and check the bright/contrast wheels for adjustment. 

8. Optionally, a recording device may be used in place of the gender changer if the device has 

both video "In" and video "Out" capabilities. 

9. Before flight, be sure to tum on the video power switch on the side of the fuselage/pod and 

ensure a good signal is being received. 

10. The MUX camera to camera switch is the short toggle near the shutter trigger switch. 

Continued 

All Content & Images Copyright© RPFlightSystems, Inc. 
P.O. Box 470 Wimberley, TX 78676 Phone: 512.847.9746 

Diversity Video System and MUX Check List. 

;-~~~- lllt.'lo~,\_. I / ,.,_ -.. , 

L LCD Monitor 2. Diversity video receiver 

3. Hi gain polarized patch anetnna 4. LCD Patch & Power Cable 

The video system includes all the following items, plus the video TX and cameras in the Spectra. The wiring is straight forward. The video RX is set to receive on channel 1, but can easily 

be switched to a different channel if required. Take note that the video patch cable has only 

two RCA jacks and one mini-stereo jack The LCD monitor has an RCA jack for video input 

from the diversity video receiver. An appropriate power plug will need to be attached to the 

LCD to meet your specific need. Setup of the video system will be as follows: 

1. Locate the video diversity receiver and insert mini stereo plug into the "AV Out" jack. 

2. Plug in a 12V power source to the diversity receiver 

3. Your diversity receiver comes with two antenna-an omni receiver for close in operations 

and high gain circular polarized patch for longer ranges. 

4. If the antennae are not attached, screw the type "F" connector from the antenna to the diversity. Either connector may be used. 

S. Locate the color LCD monitor and insert the yellow mini stereo plug into the "A V In" 

6. Plug in a 12V power source to the monitor. 

7. Plug the male (yel1ow) RCA jacks into the LCD connector box. 

8. Power up the LCD monitor and check the bright/contrast wheels for adjustment. 

9. Power up the diversity receiver by pressing the red button near the power plug 

10. Select the proper channel by pressing and releasing the power button. 

11. Optionally, a recording device may be used in between the receiver and the LCD monitor. 

Continued 

All Content & Images Copyright © RPFlightSystems, Inc. 
-------------------------------·-

P.O. Box 470 Wimberley, TX 78676 Phone: 512.847.9746 

Charger Operation 

The Triton charger included in this pack is designed to charge several different types of batteries from a 12V power 

source. This power source could be a car battery or the 11 OV AC/12VDC power supply. Most critical to this operation are the flight and video batteries. These batteries are either lithium polymer, or lithium ion in various capacities (mah) but all produce 11.1 volts nominal. A fully charged LiOn battery will show a voltage of 12.59 to 12.60 

volts. The Triton charger is defaulted to the correct values but verify that they are correct before charging. The 

LCD screen should display the following : 

· Battery Type : Li-On Voltage : 11.1 Charge rate is determined by the charger. These other values are changed by 

pushing on the round spin wheel to select the category, then rotating the wheel to change. DO NOT CHANGE 

THE ll.lVVALUE TO CHARGE LITHIUM BATTERIES! Failuretoobservethisdetailcould 

cause a fire and explosion. DO NOT CHARGE LITHIUM BATTERIES UNATTENDED either 

in a vehicle or structure' 

Use the charger by using the following steps: 

I. Connect the charger to a 12V power source. It should beep and start up automatically. 

2. Locate the "snakehead" charging adapter and insert the banana plugs in the appropriately colored jack. 

3. Connect the battery using the appropriate plug on the charging lead. 

4. Press the round spin wheel to initiate the charge sequence. The values that can be changed will flash but just 

press the button to continue to the next, and the next. 

5. The screen will change and the charger will beep-indicating that the charging sequence has started. 

6. When the battery is topped off, the unit will automatically stop charging and emit a tone. 

Battery Handling 

Lithium batteries should never be dropped, crushed, hit, folded, spindled, fondled, kneaded, mutilated or sliced in 

any way shape or form. To do so invites all sorts of ill will upon your self and your comrades. Do not over discharge a battery or try to charge it a higher rate than it can accept. If for ANY reason a battery begins to "puff up" 

and get swollen, remove it to a SAFE, NON-FLAMMABLE area for observation. 
P.O. Box 470 Wimberley, TX 78676 Phone: 512.847.9746 

Activating the Thermal Stabilization System 

(optional) 

Missions may be flown successfully without the use of the thennal stabilization system if so desired. The thermal 

stabilization helps damp out some of the effects of wind and helps reduce the load on the pilot by keeping the aircraft in level flight. When the system is engaged, it should be noted that the more stabilization used, the more control input is required from the ground control station to affect the aircraft. There are some restrictions to its use, 

the most common times NOT to use the system is : 

1. During dense fog or heavy overcast 

2. Over water 

3. Over snow 

The system will advise you through of flight integrity through the calibration process by activating a single control 

elevon from 1 to 10 times. 1 being the least amount of integrity, and 10 being the optimum. To calibrate the thermal stabilization system perform he following steps : 

1. After power up of all systems, and just before launch, point the nose of the aircraft straight toward the ground 

2. Maintain at least 50 feet from trees, cars or nearby buildings. 

3. Calibrate the unit over grass. Do not calibrate over asphalt or concrete as heat reflected from these surfaces 

will cause the thermal sensor to respond inappropriately. 

4. Press and hold the red "CAL" button on top of the cowling until one control surfaces activates. 

5. Release the calibration button while maintaining the nose down condition. 

6. The system will indicate calibration level by activating the elevon a number of times. We do NOT recommend the use of the thennal stabilization system unless you get a return of 4 or activations or better. 

7. Once the calibration is complete, hold the aircraft upright and move the right stick on the ground control unit. 

You are ready to launch 

8. The thermal stabilization system is activated by turning the center knob on the face of the GCUto the right 

9. The degree of control can be "dialed in" by varying the center point of the knob. For instance, turning the 

knob all the way to the right is 100% stabilization, turning the knob only half way gives 50% stabilization. 

lO.DO NOT ATTEMPf TO LAUNCH YOUR AIRCRAFT WITH THE STABILIZATION SYSTEM ENGAGED! 

11. Once your aircraft is at a safe altitude, activate the system and test by starting a gentle turn and releasing the 

sticks. The aircraft should right it'lelf 

12. The stabilization system may be used to assist in landings. Once lined up with the landing zone, the aircraft 

may allowed to land itself 

13. Once the system is calibrated, it should be good for the duration of the days flying. If weather conditions 

should change drastically, then the unit should be re-calibrated. 

Appendix "B" 

Motion Picture and Television Operations Manual 

41Page 

Q~DRONE C~~ i DYNAMICS 

Motion Picture and Television 

Flight Operation Manual 

Drone Pilot LLC 

PO BOX 5756 • Austin, Texas 78763 

{512) 580-5100 
c. 
1. Introduction 

A. Purpose 

(4~) DRON:E 

() . DYNAMICS 

This manual has been developed by "Drone Dynamics LLC", hereafter referred to 

as "Drone Dynamics", in conjunction with an exemption under Section 333 of 

Public Law 112-95 in reference to 49 U.S.C. § 44704 for the purposes of filming. 

Drone Dynamic's pilots and other company personnel when applicable will comply 

with the policies, procedures and conditions of this manual, whenever motion 

picture or television flight operations are performed that require a Waiver of 

Authorization as mentioned above. 

B. Operator Organization 

Drone Dynamics LLC 

PO Box 5756 

Austin, TX 78773-5756 

( 512) 580-51 00 office 

C. Persons Authorized 

The certificate holder shall ensure that no persons are allowed within 500 feet of 

the area except those consenting to be involved and necessary for the filming 

production. This provision may be reduced to no less than 200 feet if an 

equivalent level of safety can be achieved and the Administrator has approved it. 

For example, an equivalent level of safety may be determined by an ASI's 

evaluation of the filming production area to note terrain features, obstructions, 

buildings, etc. Such barriers may protect nonparticipating persons (observers, the 

public, news media, etc.) from debris in the event of an accident. 

D. Area of Operations 

Drone Dynamics' approved area of operations will be the United States. 
·' 
E. Plan of Activities 

At least three (3) days prior to any scheduled filming, Drone Dynamics will submit 

a written plan of activities to the local FSDO having jurisdiction over that area. 

The plan of activities should include the following: 

( 1) Dates and times for all flights 

(2) Name and phone number of the operator for the UAS aerial filming 

conducted under this grant of exemption 

(3) Name and phone number of the person responsible for the on-scene 

operation of the UAS 

(4) Make, model, and serial or N-Number of UAS to be used 

(5) Name and certificate number of UAS PICs involved in the aerial filming 

(6) A statement that the operator has obtained permission from property owners 

and/or local officials to conduct the filming production event; the list of those who gave 

permission must be made available to the inspector upon request 

(7) Signature of exemption holder or representative; and 

(8) A description of the flight activity, including maps or diagrams of any area, 

city, town, county, and/or state over which filming will be conducted and the altitudes 

essential to accomplish the operation. 

The three (3) day notification requirements may be waived, however, the operator 

should contact the FSDO as soon as possible with this request and be prepared to 

explain in detail why the three (3) day notification is not practical. 

F. Permission to Operate 

All operations shall be conducted over private or controlled-access property with 

permission from the property owner/controller or authorized representative. 

Permission from property owner/controller or authorized representative will be 

obtained for each flight to be conducted. Persons from whom permission may be 

required are listed below: 

(1) 

(2) 

(3) 

(4) 

(5) 

DRON: 

DYNAMiCS 

Property owners 

Law enforcement officials 

Fire department officials 

Local, State and Federal government 

Air traffic control 

Drone Dynamics personnel obtaining such permission will do so in writing 

whenever practical, however, verbal permission is acceptable otherwise. A 

standard permission form is provided in Appendix A and may be used when 

obtaining written permission. Drone Dynamics personnel will assure a sufficient 

number of those forms are available at the job site. Written permission forms will 

be maintained at the job site until flight operations are completed, and then turned 

into the pilot in command I flight supervisor to be kept on file for a minimum of six 

(6) months. These forms will be made available for inspection by the FAA or other 

official personnel upon request. 

G. Security 

Prior to any flight operation the operator will coordinate with appropriate 

production personnel to devise a plan of securing the area(s) of operation from all 

unauthorized persons and vehicles. Provisions will be made to immediately 

discontinue operations should the area(s) become unsecured or for any other 

reason in the interest of safety. 

H. Briefing of Pilot/Production Personnel 

Prior to the start of any operation under the provisions of this manual, the pilot in 

command will conduct a briefing of all procedures to participating personnel of the 

risks involved, emergency procedures, and safeguards to be followed during the 

filming production event. Personnel will also be briefed on additional provisions 

that may be issued by the FSDO that has geographic responsibility for the 

operational area, including the location of boundaries or time limits. The briefing 

shall cover: 

• Authorization for motion picture and television certificate of waiver and the 

attached special provisions 

• Operations manual 

• Plan of activities 

Clf' DRONE 

DYNAM:CS 

• Radio communications 

• UAS activities to be conducted during the filming production event 

• UAS launching procedures 

• UAS approach and landing procedures 

• Recall procedures 

• Emergency procedures 

• Risks to participating personnel 

• How to control nonparticipating persons 

I. Certification/Airworthiness 

All Drone Dynamics UAS used in operations requiring an exemption under 

Section 333 of Public Law 112-95 in reference to 49 U.S.C. § 44704, for the 

purpose of filming will be properly maintained and inspected to ensure that it is in 

a condition for safe operation. 

Prior to each flight, the PIC must conduct a pre-flight inspection and determine the 

UAS is in a condition for safe flight. The pre-flight inspection must account for all 

potential discrepancies, e.g., inoperable components, items, or equipment. If the 

inspection reveals a condition that affects the safe operation of the UAS, the 

aircraft is prohibited from operating until the necessary maintenance has been 

performed and the UAS is found to be in a condition for safe flight. 

Drone Dynamics must follow the UAS manufacturer's maintenance, overhaul, 

replacement, inspection, and life limit requirements for the aircraft and aircraft 

components. 

J. Pilot Personnel/Minimum Requirements 

The pilot/operator shall establish and specify the minimum pilot requirements. 

Minimum requirements shall meet or exceed the following: 

{1) Pilot in command must hold either an airline transport, commercial, private, 

recreational, or sport pilot certificate. The PIC must also hold a current FAA airman 

medical certificate or a valid U.S. driver's license issued by a state, the District of 

Columbia, Puerto Rico, a territory, a possession, or the Federal government. The PIC 

must also meet the flight review requirements specified in 14 CFR § 61.56 in an aircraft in 

which the PIC is rated on his or her pilot certificate. 

K. Communications 

Prior to the start of any operation covered by this manual, the pilot in command 

will formulate a plan to provide communications capability to all participants 

during the actual operation and filming. Oral, visual or radio communications may 

be used as long as it is effective and is capable of keeping the participants 

continuously appraised of the current status of the operation. 

L. Accident Notification 

Should an accident or incident requiring notification of the NTSB occur, the 

notification requirements of FAR Part 830 would comply. 

M. Recall/Stop Procedures 

Radio communication, oral, visual or a combination will be utilized to keep the 

participants continuously apprised of the current status of operation. 

N. Special Provisions 

The controls, procedures, and conditions set forth in the Drone Dynamics 

motion picture and television operations manual is the primary assurance that 

persons on the surface will not be jeopardized. 

The aircraft used under this authorization and/or waiver will only be those 

specified in attached Section 333 Exemption {"Appendix B" Page 15). Each 

pilot's name and certificate number shall appear on each daily plan of activity. All 

aircraft and pitot(s) participating in the activity shall be available for FAA 

inspection before the scheduled event. 

Each pilot-in-command conducting operations authorized under this certificate 

understands the conditions of issuance, and that it constitutes an exemption 

under Section 333 of Public Law 112-95 in reference to 49 U.S.C. § 44704. 

UAS takeoff and landing areas will be protected in a manner that will prevent 

unauthorized persons from entering the takeoff and landing area. 

Drone Dynamics will ensure that the participating persons involved in the 

operations are thoroughly briefed on special procedures, communication, 

emergency procedures, and on the provisions of the authorization and/or waiver 

before beginning the activities. No person may participate in any event unless 

that person has received a briefing on the provisions of the waiver. 

2. Company Organization 

A. Flight Supervisor I Pilot in Command 

Duties and Responsibilities: 

• Act as liaison between Drone Dynamics and the FAA on matter concerning 

this manual. 

• Assure that each approved pilot/oper~tor is issued a copy of this manual and 

obtain a signed statement from each that they have read and understand its 

contents. 

• Maintain a current copy of this manual at the main base of operations for 

Drone Dynamics. 

• Responsible for assuring that all revisions to this manual are distributed and 

processed properly. 

• Assume the responsibilities of pilot in command when acting as such. 

• May delegate functions to other personnel but retains responsibility. 

B. UAS Operator 

Duties and Responsibilities: 

• Assure that aircraft to be flown is in airworthy condition and all inspections 

and required maintenance have been performed as per section 333 

exemption. 

• Acquire permission from the flight supervisor I pilot in command before any 

operation under the provisions of this manual. 

• Be very knowledgeable of the contents of this manual and abide by the 

procedures, policies and conditions contained herein. 

• Coordinate with movie and television personnel to formulate plans, routes, 

locations, etc. with safety of all persons involved in the primary concern. 

• Maintain their copy of this manual in current condition and have it on site at 

any job or operation requiring the waiver 

C. Payload Operator 

~~)DRONE 

~/;\ DYNAMICS 

Duties and Responsibilities: 

• Assure that aircraft to be flown is in airworthy condition and all inspections 

and required maintenance have been performed as per section 333 

exemption. 

• Be very knowledgeable of the contents of this manual and abide by the 

procedures, policies and conditions contained herein. 

• Maintain their copy of this manual in current condition and have it on site at 

any job or operation requiring the waiver. 

• Coordinate with movie and television personnel to formulate shot lists. 

D. Visual Observer 

Duties and Responsibilities: 

• Be very knowledgeable of the contents of this manual and abide by the 

procedures, policies and conditions contained herein. 

• Maintain their copy of this manual in current condition and have it on site at 

any job or operation requiring the waiver. 

• Maintain visual contact with the UAS while in operation and communicate with 

the UAS operators to ensure the safety of all persons involved. 

Appendix A . 1 

C~~) DRONE 

_j DYNAMICS 

Drone Dynamics LLC 

Permission Acquisition Form 

In signing this form, I am giving the pilots of Drone Dynamics permission to operate 

their aircraft at less than 500 feet from property, or in some jurisdiction in which I am 

responsible for or affiliated with, for the purpose of film or television production. 

Name: 

Title: 

Basis of Authority to Grant Permission: 

Location: 

Date of Operation: 

Signature ----------------------

Date 

Drone Dynamics Representative Receiving Permission 

~~JDRONE (~) " DYNAMICS 

Appendix A .2 

Revision Letter 

Rev# Section Page Action Remarks Initials 

R o Remove and Replace D o Delete and Destroy N o Insert New Page 

Manual Serial# _________ lssued To ------------

Revised By ---------------

Date 

This form must be returned to the Flight Supervisor no later than ----------

Appendix B .1 · 

· (see attached Section 333 Exemption)