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Drone/UAS Practice Group 35 E Wacker Drive

Suite 1875

Chicago, IL 60601

Tel. 312.201.8310

 Jeffrey@Antonelli-Law.com

U.S. Department of Transportation August 14, 2015

Docket Management System

1200 New Jersey Ave S.E. 

Washington, D.C. 20590

Re: Request for Exemption under Section 333 of the FAA Modernization and Reform Act of 2012 

and Part 11 of the Federal Aviation Regulations from Certain Provisions of 14 C.F.R.

Seiclone Surveys, Inc.

Dear Sir or Madam:

Pursuant to Section 333 of the FAA Modernization and Reform Act of 2012 (the Reform 

Act) and 14 C.F.R. Part 11, Antonelli Law files this petition for exemption on behalf of Seiclone 

Surveys, Inc. (“Seiclone”), an operator of Small Unmanned Aircraft Systems (“UAs”) for the 

purpose of oil and gas surveying. Specifically, petitioner seeks an exemption from the Federal 

Aviation Regulations (“FARs”) listed in Appendix A to allow commercial operation of its UA, so 

long as such operations are conducted within and under the conditions outlined herein or as may 

be established by the FAA in a grant of this petition. This request is substantially similar to other 

data collection petitions previously approved, and should be considered under the expedited 

summary grant procedure.

Approval of the exemption for petitioner will allow commercial operation of the Trimble 

UX5 and UX5HP for the commercial purpose of oil and gas surveying in Class G airspace 

nationwide, or as otherwise prescribed by an Air Traffic Organization (ATO) issued COA. The 

Trimble UX5 family have been previously approved for commercial operations in the exemption 

grants listed in Section VII. The UAs covered by this petition are small battery-powered craft,

weighing approximately 6.4 lbs. (2.9 kg), inclusive of battery and payload. Operation of the UAs

under the strict conditions proposed below will provide an equivalent level of safety, as Congress 

intended, while still allowing commercial operations. Operations using these UAs are far safer 

than conventional operations conducted with helicopters and fixed-wing aircraft that weigh 

thousands of pounds, carry highly flammable fuel, and operate in close proximity to the ground, 

trees, infrastructure, and people. 

Congress directed the FAA to consider seven factors in deciding whether to approve

Section 333 exemption petitions - size, weight, speed, operational capability, proximity to airports, 

proximity to populated areas, and operation within visual line of sight. In this case, each factor 

supports the exemption request. In particular, the UAs are small, and will operate at slow speeds

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Table of Contents

I. Publishable Summary ...................................................................................................................... 5

II. Petitioner’s Contact Information.................................................................................................... 5

III. Proposed Operations........................................................................................................................ 6

A. The UAs ......................................................................................................................... 6

B. The Crew ........................................................................................................................ 7

C. Flight Conditions............................................................................................................ 7

D. Flight Operations............................................................................................................ 7

IV. Aircraft and Equivalent Level of Safety ....................................................................................... 8

VI. Proposed Conditions of the Exemption......................................................................................... 8

VI. Privacy ............................................................................................................................................. 11

VII. Public Interest and Safety................................................................................................................ 11

VIII. Regulations from Which Exemption is Requested .............................................................. 13

Appendix A: FARs as to which Seiclone wishes the same determination to be made as has 

been made previously............................................................................................................ 13
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Exhibit List

Exhibit 1: UX5 User Guide..................................................... Submitted confidentially to the FAA 

Exhibit 2: UX5 Maintenance Guide ....................................... Submitted confidentially to the FAA 

Exhibit 3: UX5 Quick Start Guide .......................................... Submitted confidentially to the FAA 

Exhibit 4: UX5 Safety Guide .................................................. Submitted confidentially to the FAA 

Exhibit 5: UX5 Instructor Pilot Manual.................................. Submitted confidentially to the FAA 

Exhibit 6: UX5 Aerial Imaging Instruction Card ................... Submitted confidentially to the FAA 

Exhibit 7: UX5 .............................................................................................................................. 16

Exhibit 8: UX5 Data Sheet ........................................................................................................... 22

Exhibit 9: UX5 White Paper ......................................................................................................... 24

Exhibit 10: UX5 HP ...................................................................................................................... 31

Exhibit 11: UX5 HP Data Sheet ................................................................................................... 36 

Exhibit 12: UX5 and UX5 HP Specifications............................................................................... 38

Exhibits 1-6 have been submitted confidentially to the FAA and are not available to the 

public.
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I. Publishable Summary

Pursuant to 14 C.F.R. §11, the following summary is provided for publication in the 

Federal Register, should it be determined that publication is needed:

Petitioner seeks an exemption from the following rules: 

14 C.F.R 21(h); 14 C.F.R. 43.7; 14 C.F.R. 43.11; 14 C.F.R. 45.11; 14 C.F.R. 45.27; 14 C.F.R. 

45.29; 14 C.F.R. 91.7(a); 14 C.F.R. 91.9(b)(2); 14 C.F.R. 91.9(c); 14 C.F.R. 91.103(b)(2); 14 

C.F.R. 91.105; 14 C.F.R. 91.109; 14 C.F.R. 91.113(b); 14 C.F.R. 91.119 (c); 14 C.F.R. 91.121; 14 

C.F.R. 91.151(a); 14 C.F.R. 91.203(a) and (b); 14 C.F.R. 91.215; 14 C.F.R. 91.403; 14 C.F.R. 

91.405(a); 14 C.F.R. 91.407(a)(1); 14 C.F.R. 409(a)(1) and (2); and 14 C.F.R. 91.417(a) and (b)

to operate commercially small unmanned aircraft systems (UAs) (6.4 lbs. or less).

Approval of the exemption requested by petitioner will allow commercial operation of the 

Trimble UX5 and UX5 HP for the purpose of oil and gas surveying in Class G airspace nationwide, 

unless otherwise prescribed by an ATO-issued COA. The requested exemption should be granted 

because operation of a small UA weighing approximately 6.4 lbs. (2.9 kg.), inclusive of battery 

and payload, conducted in the strict conditions outlined below, will provide an equivalent level of 

safety, while still allowing commercial operations. The lightweight aircraft covered by the 

exemption are far safer than conventional operations conducted with helicopters and fixed-wing 

aircraft weighing thousands of pounds and carrying highly flammable fuel, and operating in close 

proximity to the ground and people. The seven factors Congress directed the FAA to consider 

when approving Section 333 exemption petitions - size, weight, speed, operational capability, 

proximity to airports, proximity to populated areas, and operation within visual line of sight – each 

support the request. In particular, the aircraft are small, and will operate at slow speeds, and close 

to the ground. The substantial increase of safety and decrease of risk to human life, coupled with 

the low risk use of UAs to conduct these operations, weigh heavily in favor of granting the 

exemption.

II. Petitioner’s Contact Information

Aaron Totten

Owner

Seiclone Surveys, Inc.

750 Pomeroy Rd.

Eureka, MT 59917

Counsel for Petitioner:

Antonelli Law

35 E Wacker Drive

Suite 1875

Chicago, IL 60601

Tel: 312-201-8310

Email: jeffrey@antonelli-law.com
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III. Proposed Operations

A. The UAs

The requested exemption will permit petitioner to operate the Trimble UX5 and UX5HP.

The specific conditions of the proposed exemption that relate to the characteristics of the UAs are 

numbers 1, 5, and 16-20 in Section V below. Each has been adopted or imposed by the FAA in 

numerous previous grants of Section 333 exemption petitions. The UX5 and UX5 HP have the 

following specifications or equivalent:

Airframe Trimble UX5 Trimble UX5 HP

Flight Control System eBox eBox

Ground Control Station Trimble Access Aerial 

Imaging control software 

loaded onto the Trimble Tablet 

Rugged PC, which displays the 

telemetric data (including 

altitude, attitude, GPS location, 

battery power, etc.)

Trimble Access Aerial 

Imaging control software 

loaded onto the Trimble Tablet 

Rugged PC, which displays the 

telemetric data (including 

altitude, attitude, GPS location, 

battery power, etc.)

Maximum Speed 43 knots 46 knots

Maximum Take-Off 

Weight, inclusive of 

battery and technical 

payload

5.5 lbs. (2.5 kg) 6.4 lbs. (2.9 kg)

Maximum Flight Time 50 minutes 40 minutes

Transmitter muRata DNT2400P 2.4 GHz 

transmitter

muRata DNT2400P 2.4 GHz 

transmitter

Receiver internal to the eBox internal to the eBox

Propulsion System 700 W brushless motor with 

electric pusher propeller

1400 W brushless motor with 

electric pusher propeller

Data Link Internal to the Trimble Access 

Aerial Imaging control station

Internal to the Trimble Access 

Aerial Imaging control station

Batteries 14.8 V, 6,000 mAh Lithium 

Polymer battery

14.8 V, 6,600 mAh Lithium 

Polymer battery

Emergency Obstacle 

Procedure

The PIC can initiate an 

emergency landing maneuver 

to a predefined alternative 

landing zone, or abort a 

mission and cause the UA to 

safely orbit to the ground.

Should the UA lose connection 

with the ground station, it will 

return to the preset landing 

area.

The PIC can initiate an 

emergency landing maneuver 

to a predefined alternative 

landing zone, or abort a 

mission and cause the UA to 

safely orbit to the ground.

Should the UA lose connection 

with the ground station, it will 

return to the preset landing 

area.

Previously Approved 

Exemption Nos.

Exemption Nos. 11110, 11257, 

11329, 11393A, 11432, 11666, 

11806, 12231, and 12372.

Exemption Nos. 11110A and 

12231.
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B. The Crew

The crew will consist of a pilot in command (PIC) and a visual observer (VO). The PIC 

and VO will have been trained in operation of UAs generally and received up-to-date information 

on the UA to be operated pursuant to this grant. The PIC will have, at minimum, a sport pilot 

license and a U.S. driver’s license. Please refer to Exhibit 5: Instructor Pilot Manual for further 

information regarding PIC training.

The specific conditions of the proposed exemption that relate to the training and 

characteristics of the crew are numbers 3 and 6-9 in Section V below. Each has been adopted or 

imposed by the FAA in numerous previous grants of Section 333 exemption petitions. 

C. Flight Conditions

The UA will be used for oil and gas surveying in Class G airspace (unless otherwise

prescribed by an ATO-issued COA) under 400 feet above ground level (“AGL”) and under 

controlled conditions over restricted property. Petitioner will work with the local FSDO when 

planning operations. Petitioner will only operate its UA in visual meteorological conditions 

(VMC). The UA will at all times be no less than 500 feet below and no less than 2,000 feet 

horizontally from a cloud, and petitioner will not conduct operations unless visibility is at least 3 

statute miles from the PIC. The flight crew will always make a safety assessment of the risk of 

every operation, and will only operate when it is determined that no hazards are present.

For more information regarding flight conditions, please refer to Exhibit 8: UX5 Data Sheet 

and Exhibit 9: UX5 HP Data Sheet.

The specific conditions of the proposed exemption that relate to the flight conditions in 

which the UA will be operated are numbers 2, 4, 16, and 28-29 in Section V below. Each has been 

adopted or imposed by the FAA in numerous previous grants of Section 333 exemption petitions.

D. Flight Operations

The purpose of the UA flights for which exemption is requested will be for oil and gas 

surveying. Every UA flight will use at minimum a two person flight crew: a PIC and a VO. 

Petitioner will fly the UA no higher than 400 feet above ground level (AGL).

For more information regarding flight operations, please refer to the following Exhibits:

Exhibit 1: UX5 User Guide

Section 2: Planning a Project

Section 3: Preparing Equipment

Section 4: Completing a Flight

Section 5: Analysis and Export

Section 6: Troubleshooting 

Exhibit 2: UX5 Maintenance Guide

Exhibit 3: UX5 Quick Start Guide

Exhibit 4: UX5 Safety Guide

The specific conditions of the proposed exemption that relate to flight operations are 

numbers 11-12, 17-25, and 32-35 in Section V below. Each has been accepted or imposed by the 
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FAA in numerous previous grants of Section 333 exemption petitions.

IV. Aircraft and Equivalent Level of Safety

Petitioner proposes that the exemption apply to UAs that have the characteristics and that 

operate with the limitations proposed herein. These limitations provide for a level of safety at least 

equivalent to or higher than manned aircraft operations under the current regulatory structure. 

Section V below identifies the limitations and conditions to which petitioner agrees to be bound 

when conducting commercial operations under a grant of this petition. Appendix A contains a 

matrix connecting (i) the specific proposed condition with (ii) the FAR provision for which it 

provides equivalent level of safety and (iii) one or more recent Section 333 exemption grants in 

which the FAA recognized this equivalent level of safety.

Approval of the commercial operations outlined in this petition presents no national 

security issue. The PIC will possess, at minimum, a sport pilot’s certificate, so he or she will 

have been subject to security screenings by the Department of Homeland Security.

V. Proposed Conditions of the Exemption

1. The UAs, including battery and technical payload will weigh no more than approximately 6.4

lbs. (2.9 kg.).

2. UA operations under this exemption will be limited to conducting operations for the purpose 

of oil and gas surveying in Class G airspace nationwide, unless otherwise prescribed by an 

ATO issued COA.

3. Flights will be operated within line of sight of a PIC and VO.

4. Flights will be operated at an altitude of no more than 400 feet AGL, as indicated by the 

procedures specified in the operating documents. All altitudes reported to ATC must be in feet 

AGL.

5. The UA will not be flown at an indicated airspeed exceeding 46 knots.

6. Minimum flight crew for each operation will consist of the UA PIC and a VO.

7. The PIC will have at minimum a sport pilot license and either a U.S. driver’s license or a third 

class medical certificate.

8. The petitioner will not permit any PIC to operate the UA unless the PIC meets its qualification 

criteria and demonstrates the ability to safely operate the UA in a manner consistent with how 

the UA will be operated under this exemption, including evasive and emergency maneuvers 

and maintaining appropriate distances from persons, vessels, vehicles and structures. PIC 

qualification flight hours and currency will be logged in a manner consistent with 14 CFR 

§61.51(b). A record of the PIC training will be documented and made available upon request 

by the Administrator. Training operations will only be conducted during dedicated training 

sessions. During training, proficiency, and experience-building flights, all persons not essential 

for flight operations will be considered nonparticipants, and the PIC will operate the UA with 

appropriate distance from nonparticipants in accordance with 14 CFR § 91.119. 
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9. The VO will not perform any other duties beyond assisting the PIC with seeing and avoiding 

other air traffic and other ground based obstacles/obstructions, and will not be permitted to 

operate the camera or other instruments.

10. The PIC will be designated before the flight and will not be allowed to transfer his or her 

designation for the duration of the flight. The PIC will ensure that the VO can perform the 

functions prescribed in these conditions and the operating documents.

11. A briefing will be conducted in regard to the planned UA operations prior to each day’s 

activities. It will be mandatory that all personnel who will be performing duties in connection 

with the operations be present for this briefing. 

12. Prior to each flight, the PIC will inspect the UA, including the Ground Control Station, to 

ensure it is in a condition for safe flight. If the inspection reveals a condition that affects the 

safe operation of the UA, the PIC will not operate the UA until the necessary maintenance has 

been performed and the UA is found to be in a condition for safe flight. All maintenance and 

alterations will be properly documented in the aircraft records.

13. Petitioner will conduct a functional flight test on any UA that has undergone maintenance or 

alterations that affect the UA operation or flight characteristics, e.g. replacement of a flight 

critical component. The PIC who conducts the functional test flight will make an entry in the 

aircraft records. 

14. The petitioner will carry out its maintenance, inspections, and record keeping requirements, in 

accordance with the UA manufacturer’s aircraft/component, maintenance, overhaul, 

replacement, inspection, and life limit requirements set forth in the operating documents. 

Maintenance, inspection, alterations, and status of replacement/overhaul component parts will 

be noted in the aircraft records, including total time in service, description of work 

accomplished, and the signature of the authorized person returning the UA to service. The 

authorized person will make an entry in the aircraft record of the corrective action taken against 

discrepancies discovered between inspections.

15. The UA will be operated within visual line of sight (VLOS) of the PIC and VO at all times. 

This requires the PIC to be able to use human vision unaided by any device other than 

corrective lenses. PIC and VO will at all times be able to communicate verbally. They will not 

be permitted to use electronic messaging or texting to communicate during flight operations. 

16. The PIC will not begin a flight unless (considering wind and forecast weather conditions) there 

is enough power to fly at normal cruising speed to the intended landing point and prepare to 

land with at least 25% battery power remaining.

17. Actual total flight time for each operational flight will result in no less than a 25% battery 

reserve.

18. The UA will have the capability to abort a flight in case of unexpected obstacles or 

emergencies. 

19. The UA will be programmed so that if it loses communications or loses its GPS signal, it will 
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return to a pre-determined location within the planned operating area and land or be recovered 

in accordance with the operating documents.

20. If the UA and its radio control link disconnect during flight, the system’s failsafe protection 

will be triggered and the multirotor will return to home and land automatically, rather than 

flying off uncontrollably or landing at an unknown location. 

21. The operating documents required under 14 CFR §§ 91.9 and 91.203 will be maintained and 

available to the PIC at the Ground Control Station of the UA any time the UA is operating. 

These documents will be made available to the Administrator or any law enforcement official 

upon request. If a discrepancy exists between the conditions and limitations in the exemption 

grant and the procedures outlined in the operating documents, the grant conditions and 

limitations will take precedence and will be followed. Otherwise, the petitioner will follow the 

procedures outlined in its operating documents. If it updates or revises its operating documents, 

it will present updated and revised documents to the Administrator upon request. If the 

petitioner determines that any update or revision would affect the basis upon which the FAA 

granted the exemption, then the Petitioner will petition for an amendment to the grant of 

exemption. 

22. Petitioner will obtain written and/or oral permission from the landowners/authorized agents of 

the landowners over which flights will be conducted.

23. Petitioner will obtain all required permissions and permits from territorial, state, county or city 

jurisdictions, including local law enforcement, fire, or other appropriate governmental 

agencies. 

24. UA operations will not be conducted during night, as defined in 14 CFR § 1.1. All operations 

will be conducted under visual meteorological conditions (VMC). Flights will not be 

conducted under special visual flight rules (SVFR). 

25. The petitioner will obtain an Air Traffic Organization (ATO) issued Certificate of Waiver or 

Authorization (COA) prior to conducting any operations under the grant of exemption. 

Petitioner will request a Notice to Airman (NOTAM) not more than 72 hours in advance, but 

not less than 24 hours prior to the operation. All operations will be conducted in accordance 

with airspace requirements in the ATO issued COA, including class of airspace, altitude level 

and potential transponder requirements. 

26. The UA will not be operated within 5 nautical miles of an airport reference point as denoted 

on a current FAA-published aeronautical chart unless a letter of agreement with that airport’s 

management has been obtained, and the operation is conducted in accordance with a NOTAM 

as required by the operator’s COA. Any letter of agreement with the airport management will 

be made available to the Administrator upon request. 

27. The UA will not be operated less than 500 feet below, or less than 2,000 feet horizontally from, 

a cloud or when visibility is less than 3 statute miles from the PIC. 

28. All operations shall be conducted in Class G airspace or as otherwise prescribed in an ATO 

issued COA. 
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29. All aircraft operated in accordance with this exemption will be identified by serial number, 

registered in accordance with 14 CFR part 47, and have identification (N-Number) markings 

in accordance with 14 CFR part 45, Subpart C. Markings will be as large as practicable. 

30. Before conducting operations, petitioner will ensure that the radio frequency spectrum used 

for operation and control of the UA complies with the Federal Communications Commission 

(FCC) or other appropriate government oversight agency requirements. 

31. The UA will remain clear and yield the right of way to all manned aviation operations and 

activities at all times. 

32. The UA will not be operated by the PIC from any moving device or vehicle. 

33. Petitioner will conduct all flight operations at least 500 feet from all nonparticipating persons, 

vessels, vehicles, and structures unless one of the following three conditions is met:

a. Barriers or structures are present that sufficiently protect nonparticipating persons from the 

UA and/or debris in the event of an accident. The petitioner will ensure that 

nonparticipating persons remain under such protection. If a situation arises where 

nonparticipating persons leave such protection and are within 500 feet of the UA, the PIC 

will ensure that flight operations cease immediately.

b. The aircraft is operated near vessels, vehicles or structures where the owner/controller of 

such vessels, vehicles or structures has granted permission and the PIC has made a safety 

assessment of the risk of operating closer to those objects and determined that it does not 

present undue hazard.

c. Operations nearer to the PIC, VO, operator trainees or essential persons do not present an 

undue hazard to those persons per § 91.119(a).

34. Petitioner will report any incident, accident, or flight operation that transgresses the lateral or 

vertical boundaries of the operational area as defined by the applicable COA to the FAA's UAS 

Integration Office (AFS-80) within 24 hours. Petitioner will report accidents to the National 

Transportation Safety Board (NTSB) per instructions contained on the NTSB Web site: 

www.ntsb.gov.

VI. Privacy

There is little concern that the proposed flights will cause invasions of privacy. All flights 

will occur over either (a) public rights of way where there is no expectation of privacy; or (b) over 

private property with permission of the landowner/authorized agent and consent of participating 

individuals.

VII. Public Interest and Safety

The planned UA use will increase ground safety for aerial oil and gas surveying operations. 

This type of data collection has previously been done by manned aircraft or by individuals on the 

ground. Both are more time consuming and are more expensive than using a UA. Use of manned 

aircraft poses enhanced risk to the pilot and onboard crew, who would be several hundred feet in 
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the air. 

The enhanced safety and reduced environmental impact achieved using a UA and carrying 

no passengers or crew, rather than a manned aircraft of significantly greater proportions, carrying 

crew in addition to flammable fuel, gives the FAA good cause to find that the UA operation 

enabled by this exemption is in the public interest.

Satisfaction of the criteria provided in Section 333 of the Reform Act of 2012 – size, 

weight, speed, operating capabilities, proximity to airports and populated areas and operation 

within visual line of sight and national security – provide more than adequate justification for the 

grant of the requested exemption allowing commercial operation of petitioner’s UA in the utility 

and infrastructure inspection industries, pursuant to Seiclone’s rules of operation.

The FAA has previously approved the UX5 family for commercial operations in 

Exemption Nos. 11110 and 11110A, 11257, 11329, 11393A, 11432, 11666, 11806, 12231, and 

12372. 

Additionally, the FAA has previously approved comparable UAs for oil and gas industry 

operations in Exemption Nos. 

11176 (oil and gas facility monitoring); 

11208 (oil and gas platform inspections); 

11252 (oil and gas industry inspections); 

11355 (oil and gas exploration, pipeline inspection);

11422 (oil and gas pipeline inspections);

11524 (oil and gas pipeline inspections);

11525 (oil and gas pipeline inspections);

11886 (commercial operations for oil and gas);

11929 (oil and natural gas pipeline inspections); and 

11953 (oil and gas facility inspections).
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VIII. Regulations from Which Exemption is Requested

Appendix A: FARs as to which Seiclone wishes the same determination to be made as has 

been made previously.

FAR 

Provision

Applicable condition(s) in 

Section 5 of petition

FAA Exemption Decision

21(h) 1, 2, 3, 4, 5, 16, 25, 28, 29 Nos. 11062, 11063, 11064, 11065, 11066, 11067, 

11080, 11109, 11111, 11110, 11114, 11136, 11138, 

11150, 11153, 11156, 11157, 11166, 11167, 11170, 

11171, 11172, 11174, 11176, 11177, 11178, 11184, 

11185, 11188, 11189, 11191, 11192, 11193, 11195

43.7 13, 14 No. 11208

43.11 12 No. 11208

45.11 29 No. 11208

45.27 29 No. 11188

45.29 29 Nos. 11136, 11157, 11170, 11185, 11193

91.7(a) 12 Nos. 11062, 11063, 11064, 11065, 11066, 11067, 

11080, 11109, 11110, 11136, 11138, 11150, 11153, 

11156, 11157, 11158, 11160, 11161, 11166, 11167, 

11170, 11171, 11172, 11174, 11177, 11178, 11184, 

11185, 11188, 11189, 11191, 11192, 11193, 11195, 

11204

91.9(b)(2) 22 Nos. 11062, 11063, 11064, 11065, 11066, 11067, 

11080, 11109, 11110, 11111, 11112, 11114, 11136, 

11138, 11150, 11153, 11156, 11157, 11062, 11063, 

11064, 11065, 11066, 11067, 11080, 11109, 11110, 

11111, 11112, 11114, 11136, 11138, 11150, 11153, 

11156, 11157, 11174, 11177, 11178, 11184, 11185,

11189, 11192, 11193, 11195

91.9(c) 30 Nos. 11136, 11170, 11171, 11174, 11185

91.103(b)(2) 3, 9, 15, 16, 17, 18, 19, 20 Nos. 11062, 11063, 11064, 11065, 11066, 11067, 

11080, 11109, 11138, 11150, 11153, 11156, 11158, 

11160, 11161, 11166, 11167, 11171, 11172, 11176, 

11177, 11178, 11184, 11185, 11188, 11188, 11189, 

11191, 11192, 11193, 11195, 11204

91.105 6 No. 11185 

91.109 7, 8 Nos. 11062, 11063, 11064, 11065, 11066, 11067, 

11080, 11109, 11110, 11112, 11136, 11138, 11150, 

11153, 11156, 11157, 11166, 11167, 11170, 11171, 

11174, 11177, 11184, 11185, 11189, 11191, 11192, 

11193, 11194, 11195, 11206, 11208

91.113(b) 3, 31 No. 11238
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FAR 

Provision

Applicable condition(s) in 

Section 5 of petition

FAA Exemption Decision

91.119(c) 4, 33 Nos. 11162, 11163, 11164, 11165, 11166, 111080, 

111109, 11110, 11111, 11112, 11114, 11136, 

11138, 11150, 11153, 11156, 11160 11161, 11166, 

11167, 11170, 11171, 11172, 11174, 11176, 11178, 

11185, 11188, 11189, 11190, 11193

91.121 4 Nos. 11162, 11163, 11164, 11165, 11166, 111080, 

111109, 11136, 11138, 11150, 11153, 11156, 11160 

11161, 11166, 11167, 11170, 11171, 11174, 11176, 

11178, 11185, 11188, 11189, 11190, 11193

91.151(a) 16, 17 Nos. 11110, 11153, 11156, 11161; 111109, 11110, 

11112, 11136, 11138, 11150, 11153, 11156, 11160 

11161, 11166, 11167, 11170, 11171, 11172, 11174, 

11176, 11178, 11185, 11188, 11189, 11190, 11193

91.203 (a) 

and (b)

22 Nos. 11062, 11063, 11064, 11065, 11066,

11067, 11080, 11109, 11110, 11111, 11112,

11114, 11136, 11138, 11150, 11153, 11156,

11157, 11170, 11171, 11172, 11174, 11176,

11177, 11178, 11184, 11185, 11188, 11188,

11189, 11191, 11192, 11193, 11195

91.215 25, 26 No. 11185, 11195

91.403 12, 13, 14 No. 11185

91.405(a) 12, 13, 14 Nos. 11062, 11063, 11064, 11065, 11066,

11067, 11080, 11109, 11110, 11111, 11112,

11114, 11136, 11138, 11150, 11153, 11156,

11157, 11158, 11160, 11161, 11166, 11167,

11170, 11171, 11172, 11174, 11176, 11177,

11178, 11184, 11185, 11188, 11188, 11189,

11191, 11192, 11193, 11195, 11204

91.407(a)(1) 14 Nos. 11062, 11063, 11064, 11065, 11066,

11067, 11080, 11109, 11110, 11111, 11112,

11114, 11136, 11138, 11150, 11153, 11156,

11157, 11158, 11160, 11161, 11166, 11167,

11170, 11171, 11172, 11174, 11176, 11177,

11178, 11184, 11185, 11188, 11188, 11189,

11191, 11192, 11193, 11195, 11204

91.409(a)(1) 12, 13, 14 Nos. 11062, 11063, 11064, 11065, 11066,

11067, 11080, 11109, 11110, 11111, 11112,

11114, 11136, 11138, 11150, 11153, 11156,

11157, 11158, 11160, 11161, 11166, 11167,

11170, 11171, 11172, 11174, 11176, 11177,

11178, 11184, 11185, 11188, 11188, 11189,

11191, 11192, 11193, 11195, 11204
15

FAR 

Provision

Applicable condition(s) in 

Section 5 of petition

FAA Exemption Decision

91.409(a)(2) 12, 13, 14 Nos. 11062, 11063, 11064, 11065, 11066,

11067, 11080, 11109, 11110, 11111, 11112,

11114, 11136, 11138, 11150, 11153, 11156,

11157, 11158, 11160, 11161, 11166, 11167,

11170, 11171, 11172, 11174, 11176, 11177,

11178, 11184, 11185, 11188, 11188, 11189,

11191, 11192, 11193, 11195, 11204

91.417(a) 12, 13, 14 Nos. 11062, 11063, 11064, 11065, 11066,

11067, 11080, 11109, 11110, 11111, 11112,

11114, 11136, 11138, 11150, 11153, 11156,

11157, 11158, 11160, 11161, 11166, 11167,

11170, 11171, 11172, 11174, 11176, 11177,

11178, 11184, 11185, 11188, 11188, 11189,

11191, 11192, 11193, 11195, 11204

91.417(b) 12, 13, 14 Nos. 11062, 11063, 11064, 11065, 11066,

11067, 11080, 11109, 11110, 11111, 11112,

11114, 11136, 11138, 11150, 11153, 11156,

11157, 11158, 11160, 11161, 11166, 11167,

11170, 11171, 11172, 11174, 11176, 11177,

11178, 11184, 11185, 11188, 11188, 11189,

11191, 11192, 11193, 11195, 11204
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UX5 HP UX5 faa exemption specifications user stories flight calculator

Take mapping to a new level and

 beyond

Engineered to help mapping and surveying professionals who require

 the highest accuracy work more efficiently, the Trimble UX5 sets the

 standard in mapping and surveying by combining a robust and highly

 user-friendly system with a custom-designed camera that offers the

 most impressive deliverables. The Trimble UX5 keeps you productive

 all day long - whatever job you're working on.

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UX5

LEADING IMAGE

 ACQUISITION

 QUALITY AND

 DATA

 ACCURACY

ALL-TERRAIN

 AND ALLWEATHER

 PERFORMANCE

REVERSE

 THRUST FOR

 PRECISE

 LANDINGS IN

 CONFINED

 SPACES

DURABLE AND

 RELIABLE

 SOLUTION FOR

 INTENSIVE USE

FULLY

 AUTOMATED

 TRIMBLE

 ACCESS

 WORKFLOWS

 FOR EASE- OFUSE

16
17
Leading image acquisition

 quality and data accuracy 

Designed to follow the latest developments

 in the ‘prosumer’ camera market, the

 Trimble UX5 ensures optimal image quality

 along with maximum photogrammetric

 accuracy. The UX5 camera has – unlike a

 traditional compact camera – a large

 imaging sensor that captures very sharp,

 color-rich images, even in dark or cloudy

 conditions. The 24 MP camera and its

 custom optics give the UX5 the ability to

 capture data down to 2.0 cm (0.79 in)

 resolution.

All-terrain and all-weather

 performance 

The remarkable design of the Trimble UX5

 ensures employability nearly everywhere

 and in practically all weather conditions.

 Whether you choose to fly in rainy

 conditions along windy seashores, in hot

 deserts, or in a snowy, mountain terrain, the

 Trimble UX5 is a dependable solution to

 gather high quality data without

 compromising coverage.

Reverse thrust for precise

18
 landings in confined spaces

The Trimble UX5 overcomes the limitations

 of traditional UAS landings with the addition

 of an advanced control method. Based on

 reversed thrust, this innovative improved

 altitude measurement results in accurate

 and predictable landings for landing

 confidence every time. For professionals

 working in small areas, the landing angle

 and trajectory is compact and allows

 landings in confined spaces.

Durable and reliable solution

 for intensive use 

Based on a production method patented by

 Trimble, the Trimble UX5 combines an

 impact resistant foam structure and internal

 and external composite elements that give

 the UX5 its extreme durability and strength.

 Additionally, the design focus has been on

 delivering an easy to maintain airframe that

 can be renewed at users’ discretion by a

 plug-and-play fitting of the protected internal

 electronics.

Fully automated Trimble

 Access workflows for ease-

 of-use 

The Trimble Access Aerial Imaging

 application loaded onto the Trimble Tablet

 Rugged PC operates the Trimble UX5 and

19
 is a single software tool for planning

 your aerial missions, performing pre-flight

 checks and monitoring your flights – all with

 intuitive workflows that ensure reliable

 results. In the field, the operator is guided

 through the pre- and post-flight sequences

 with step-by-step digital checklists. For

 additional time and resource savings, many

 of the Trimble UX5 checks are automatically

 verified by the software and do not require

 any interaction from the operator. Plus, the

 fast and intuitive workflow allows the

 Trimble UX5 to be ready to fly in only 5

 minutes ensuring minimal downtime.

NEWSLETTER SUBSCRIPTION

#WORLDELEPHANTDAY: READ HOW...

 RT @EMISONTECH: LOVE MY NEW...

@EMISONTECH GLAD YOU ARE ENJOYING YOUR NEW...

TRIMBLE NAVIGATION LIMITED, GENT, BELGIUM DISCLAIMER SITEMAP DESIGNED & DEVELOPED BY XIO

20
21
Trimble UX5 Unmanned Aircraft System

THE STANDARD IN MAPPING 

AND SURVEYING

The Trimble® UX5 Unmanned Aircraft System 

(UAS) sets the standard for fast and safe aerial 

data collection by offering a complete system 

with powerful technologies such as a robust 

design, a radically simplified workflow and 

reversed thrust & automatic failsafe procedures. 

The Trimble UX5 offers a much safer method to 

collect data compared to traditional surveying 

methods. Featuring the Trimble AccessTM Aerial 

Imaging application, flights are conducted in a 

fully automated manner, from launch to landing, 

and require no piloting skills. The Trimble UX5 

makes a once time consuming and complex 

process incredibly easy – no matter what 

the conditions. 

Superior Image Acquisition

The Trimble UX5 ensures optimal image quality 

along with maximum photogrammetric accuracy. 

The camera has a large imaging sensor that 

captures very sharp, color-rich images, even in 

dark or cloudy conditions. The 24 MP camera 

and its custom optics give the UX5 the ability to 

capture data down to 2 cm (0.79 in) resolution.

Unrivaled Performance 

Based on a production method patented by 

Trimble, the Trimble UX5 combines an impact 

resistant foam structure and internal and external 

composite elements that give the UX5 its extreme 

durability and strength. Additionally, the design 

focus has been on delivering an easy to maintain 

airframe that can be renewed at users’ discretion 

by a plug-and-play fitting of the protected 

internal electronics. 

The remarkable design of the Trimble UX5 

ensures employability nearly everywhere and in 

practically all weather conditions. Whether you 

choose to fly in rainy conditions along windy 

seashores, in hot deserts, or in a snowy, mountain 

terrain, the Trimble UX5 is a dependable 

solution to gather high quality data without 

compromising coverage.

Landings, less space – more accurate

The Trimble UX5 overcomes the limitations 

of traditional fixed wing UAS landings with 

the addition of an advanced control method. 

Based on reversed thrust, this improved altitude 

measurement results in accurate and predictable 

landings for landing confidence every time. For 

professionals working in small areas, the landing 

angle and trajectory is compact and allows for 

landings in confined spaces.

Intuitive Workflows with 

Trimble Access

The Trimble Access Aerial Imaging application 

loaded onto the Trimble Tablet Rugged PC 

operates the Trimble UX5 and is a single software 

tool for planning your aerial missions, performing 

pre-flight checks and monitoring your flights – 

all with intuitive workflows that ensure reliable 

results. In the field, the operator is guided 

through the pre- and post-flight sequences 

with step-by-step digital checklists. The fast 

and intuitive workflow allows the Trimble UX5 

to be ready to fly in only 5 minutes ensuring 

minimal downtime.

Valuable Photogrammetry Deliverables

Optimized to process data from the Trimble 

UX5 Unmanned Aircraft System, the Trimble 

Business Center Photogrammetry Module 

creates impressive deliverables. Produce point 

clouds, Triangulated Irregular Network (TIN) 

models and contour maps of the area flown. 

These can then be used to calculate volumes, 

excavation planning, drainage planning and many 

other functions. Trimble Business Center also 

produces a scaled orthophoto of the area that 

can be used to plan a project, define features of 

interest, identify property boundaries, or show 

construction progress by comparing orthophotos 

from different times.

Key Features 

Leading image acquisition quality and 

data accuracy

All-terrain and all-weather performance 

Reverse thrust for precise landings in 

confined spaces

A durable and reliable solution for 

intensive use

Fully automated Trimble Access workflows for 

ease-of-use and safe operation

Simple data processing with Trimble 

Business Center photogrammetry module

DATASHEET

22
OPERATION

Endurance1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 50 minutes

Range1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 60 km (37.28 mi)

Cruise speed. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 80 kmh (50 mph)

Maximum ceiling2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5000 m (16,404 ft)

Pre-flight system setup time. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 minutes

Take off

Type. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Catapult launch

Angle. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 30 degrees

Landing

Type. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Belly landing

Angle. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14 degrees

Landing space (L x W)2

Typical. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 m x 6 m (66 ft x 20 ft)

Recommended. . . . . . . . . . . . . . . . . . . . . . . . . . 50 m x 30 m (164 ft x 98 ft)

Weather limit. . . . . . . . . . . . . . . . . . . . . . . . . 65 kmh (40.39 mph) and light rain

Communication & control frequency. . . . . . . . . . . . . . . . . . . . . . . 2.4 GHz (FHSS)

Communication & control range. . . . . . . . . . . . . . . . . . . . . Up to 5 km (3.10 mi)

ACQUISITION PERFORMANCE

Resolution (GSD). . . . . . . . . . . . . . . . . . . . . 2.0 cm to 19.5 cm (.79 in to 7.67 in)

Height above take-off location (AGL). . . . . . . 75 m to 750 m (246 ft to 2,460 ft)

AREA COVERAGE TABLE

Height GSD Coverage/flight [km2] (1) Coverage/day [km2] (2)

70% 80% 90% 70% 80% 90%

75 m

(246 ft)

2.0 cm

(0.79 in)

1.1 km2

(0.43 mi2)

0.8 km2

(0.31 mi2)

0.4 km2

(0.15 mi2)

6.85 km2

(2.63 mi2)

4.5 km2

(7.74 mi2)

2.3 km2

(0.88 mi2)

100 m

(328 ft)

2.6 cm

(1.02 in)

1.8 km2

(0.7 mi2)

1.2 km2

(0.64 mi2)

0.6 km2

(0.23 mi2)

10.8 km2

(4.17 mi2)

7.2 km2

(2.78 mi2)

3.6 km2

1.39 mi2)

150 m

(492 ft)

3.9 cm

(1.54 in)

3.1 km2

(1.2 mi2)

2.1 km2

(0.81 mi2)

1.0 km2

(0.39 mi2)

18.7 km2

(7.22 mi2)

12.5 km2

(4.83 mi2)

6.2 km2

(2.39 mi2)

200 m

(656 ft)

5.2 cm

(2.05 in)

4.4 km2

(1.7 mi2)

3.0 km2

(1.16 mi2)

1.5 km2

(0.58 mi2)

26.6 km2

(10.27 mi2)

17.8 km2

(6.87 mi2)

8.9 km2

(3.44 mi2)

250 m

(820 ft)

6.5 cm

(2.56 in)

5.8 km2

(2.24 mi2)

3.8 km2

(1.47 mi2)

1.9 km2

(0.73 mi2)

34.6 km2

(13.36 mi2)

23.1 km2

(8.92 mi2)

11.5 km2

(4.44 mi2)

300 m

(984 ft)

7.8 cm

(3.07 in)

7.1 km2

(2.74 mi2)

4.7 km2

(1.81 mi2)

2.4 km2

(0.93 mi2)

42.5 km2

(16.41 mi2)

28.3 km2

(10.93 mi2)

14.2 km2

(5.48 mi2)

400 m

(1,312 ft)

10.4 cm

(4.09 in)

9.7 km2

(3.75 mi2)

6.4 km2

(2.47 mi2)

3.2 km2

(1.24 mi2)

58.0 km2

(22.40 mi2)

38.7 km2

(14.94 mi2)

19.3 km2

(7.45 mi2)

500 m

(1,640 ft)

13 cm

(5.12 in)

12.4 km2

(4.79 mi2)

8.2 km2

(3.17 mi2)

4.1 km2

(1.58 mi2)

74.2 km2

(28.65 mi2)

49.5 km2

(19.11 mi2)

24.7 km2

(9.54 mi2)

750 m

(2,461 ft)

19.5 cm

(7.67 in)

19.0 km2

(7.34 mi2)

12.7 km2

(4.90 mi2)

6.3 km2

(2.43 mi2)

113.9 km2

(43.98 mi2)

75.9 km2

(29.31 mi2)

38.0 km2

(14.67 mi2)

(1) For a 2:1 aspect ratio, which is a flight block with length equal to 2 times the width. This is a good approximation of

the average flight block.

(2) Assuming on average 5 minutes pre-flight and 5 minutes post-flight setup and recovery time and operation between 

10 am and 4 pm.

PERFORMANCE SPECIFICATIONS

• Maximized image footprint without compromising resolution, obtained with 

a custom wide-angle lens and APSC-type sensor.

• Maximized coverage per flight and per hour due to large image footprint, 

sharp turning capability and high cruise speed.

• Reversed thrust technology for a short and steep landing circuit.

• Powerful propulsion system for steep climbs and high altitude flights.

• High airframe service life due to wing robustness and maintainability.

• Short setup time with automated procedures in Trimble Access field software.

• Self-check and failsafe procedures for safe operation.

• One-button export to Trimble Business Center to create deliverables.

• Optimized data accuracy when processed with Trimble Business Center.

HARDWARE

Type. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Fixed wing

Weight. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.5 kg (5.51 lb)

Wingspan. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 m (3.28 ft)

Wing area. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 34 dm

Dimensions. . . . . . . . . 100 cm x 65 cm X 10.5 cm (39.37 in x 25.59 in x 4.13 in)

Material. . . . . . . . . . . . . EPP foam; Carbon frame structure; Composite elements

Propulsion. . . . . . . . . . . . . . . . . Electric pusher propeller; brushless 700 W motor

Battery. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.8 V, 6000 mAh

Camera. . . . . . . . . . . . . . . . . . . 24 MP mirrorless APSC with custom 15 mm lens

Controller. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Trimble Tablet Rugged PC

SOFTWARE

Trimble Access Aerial Imaging application

• Project management

• Mission planning with option for multiple flights

• Automated pre-flight checks

• Automatic take off, flight and landing

• Autonomous camera triggering

• Automated fail-safe routines

• User controlled fail-safe commands

• Automated data consistency checks

• Export to Trimble Business Center and a generic format for image processing

Specifications subject to change without notice.

© 2013–2015, Trimble Navigation Limited. All rights reserved. Trimble and the Globe & Triangle logo are trademarks of Trimble 

Navigation Limited, registered in the United States and in other countries. Access is a trademark of Trimble Navigation Limited. All 

other trademarks are the property of their respective owners. PN 022543-576B (06/15)

1 ISO standard atmosphere conditions.

2 1 sigma for wind <30 kph (19 mph).

DATASHEET

Trimble UX5 Unmanned Aircraft System

TRIMBLE AUTHORIZED DISTRIBUTION PARTNER

NORTH AMERICA

Trimble Navigation Limited

10368 Westmoor Dr

Westminster CO 80021

USA

EUROPE

Trimble Germany GmbH

Am Prime Parc 11

65479 Raunheim 

GERMANY

ASIA-PACIFIC

Trimble Navigation 

Singapore Pty Limited

80 Marine Parade Road

#22-06, Parkway Parade

Singapore 449269 

SINGAPORE

23
ABSTRACT

Using Unmanned Aircraft Systems (UAS) for photogrammetric 

aerial mapping provides surveyors and other geospatial 

professionals with a revolutionary tool for collecting data 

that was once reserved for large photogrammetry specialists. 

Trimble is creating the standard for Aerial Imaging Solutions by 

simplifying a once complex and time-consuming process. Aerial 

Imaging Solutions allow survey and geospatial professionals to 

collect large amounts of data (several square kilometers) in a 

short time (less than one hour) from a safe location for use in 

a variety of applications – rapid, safe, flexible.

WHITE PAPER

Dr P. Cosyn & R. Miller

Trimble Survey, Westminster, CO, USA 

Survey & Engineering Division, 10368 Westmoor Drive, Westminster, CO 80021-2712, USA

© 2013, Trimble Navigation Limited. All rights reserved. Trimble, the Globe & Triangle logo, Trimble Access are trademarks of Trimble Navigation Limited, registered in the United States Patent and 

Trademark Office and in other countries. All other trademarks are the property of their respective owners. Last updated May 2013. PN 022543-549 (09/12)

Trimble’s UX5 Aerial Imaging Solution is an ideal and innovative 

tool that can be utilized for survey, open-pit mine, oil & gas, 

landfill, and environmental applications such as; topographic 

surveys, site & route planning, progress monitoring, volume 

calculations, disaster analysis and as-builts, along with a wide 

variety of other applications.

TRIMBLE UX5 AERIAL IMAGING SOLUTION

A new standard in accuracy, robustness and performance 

for photogrammetric aerial mapping

WWW.TRIMBLE.COM/UAS

24
INTRODUCTION

Digital imaging is a rapidly expanding and highly valuable 

technology for geospatial professionals. Imagery is often 

used to visualize job site conditions, review survey & mapping 

observations, measure points & features, and create twodimensional & three-dimensional deliverables. In some cases, 

the imagery itself could be the desired deliverable. Imaging 

can be accomplished from both the terrestrial perspective 

as well as the aerial perspective. Both terrestrial panoramic 

and overhead point-of-views have advantages for given 

applications. The aerial perspective is optimal for documenting 

and measuring large horizontal sites, while the terrestrial 

perspective is ideal for documenting and measuring vertical 

structures such as buildings and bridges. Because many sites 

have a combination of both horizontal and vertical objects 

that need to be surveyed, there is a benefit to collecting both 

forms of imagery and merging them. 

Trimble prides itself on being a leader in innovation. By setting 

new industry standards to improve our users’ efficiencies and 

deliverables, we are proud to provide even more breadth and 

depth to our portfolio by offering the first and only complete 

Aerial Imaging Solution specifically designed for surveyors 

and geospatial professionals. The system is comprised of 

the Trimble UX5 Aerial Imaging Rover for collecting aerial 

photography; Trimble AccessTM Aerial Imaging application 

for mission planning, pre-flight checks and flight monitoring; 

and Trimble Business Center Photogrammetry module for 

processing aerial images and creating deliverables. This white 

paper discusses Trimble’s complete UAS photogrammetric 

mapping solution and simplified deliverable generation that 

make it the preferred solution for any demanding aerial 

surveying or mapping task.

IMAGE ACQUISITION METHODOLOGY

Being successful with aerial mapping is predicated on the 

planning of flights and the desired deliverables. The typical 

phases for image acquisition are:

f Mission planning: In the office (and in the field) users can 

define the mission area, add background maps, and define 

avoidance zones if required. The software estimates the total 

flight time needed to cover the mission area and allows the 

user to split the area into multiple flights when required 

because of the size of the area. 

f Flight planning: For each flight, the pilot identifies the wind 

direction, takeoff location, and the landing location, so that 

the duration of the flight can be re-calculated based on the 

field conditions at the time of the flight. The launcher is set 

up and the pre-flight checklist is completed to ensure that the 

system is ready for flight. 

f Flight operation: After launching the Trimble UX5 Aerial 

Imaging Rover, the flight is monitored using the ground 

control station. No manual interventions are required unless 

the user wants (or needs) to abort the flight. After the Trimble 

UX5 Aerial Imaging Rover lands, the post-flight checklist is 

completed to transfer the data to the computer.

f Analysis: This process allows for a completeness check of the 

data. It ensures that the user is confident that he heads home 

with data he can process to his deliverables.

FIGURE 2 Trimble AccessTM mission operation

FIGURE 1 Trimble AccessTM mission planning

DELIVERABLES

Orthophotos, contour maps, three-dimensional (3D) photos, 

point clouds, digital surface models (DSMs), and feature 

maps can easily be created from aerial imagery from Trimble 

Business Center. Trimble has created a new standard for 

processing UAS aerial imagery by incorporating more than 30 

years of experience in photogrammetry from Inpho, a Trimble 

software solution, into streamlined workflows in the recently 

released Trimble Business Center Photogrammetry module.

WWW.TRIMBLE.COM/UAS 2

25
FIGURE 4 Contour map produced with Trimble Business Center 

Photogrammetry module

FIGURE 6 Panorama image in Trimble Business Center, taken with the 

Trimble VX Spatial Station

FIGURE 5 3D image colored by elevation produced with Trimble 

Business Center Photogrammetry module

FIGURE 7 True-color point cloud in Trimble RealWorks, taken with the 

Trimble TX5 3D Laser Scanner

measurements can be taken from, but this type of data cannot 

be used to measure vertical structures such as buildings or 

bridges. By combining data collected with Trimble’s leading 

edge vision technology, such as the Trimble UX5 Aerial 

Imaging Rover, Trimble VX Spatial Station, and Trimble TX5 3D 

Laser Scanner, users can visualize their project from multiple 

perspectives, measure points within the images and create 3D 

models of the infrastructure and terrain.

FIGURE 3 Orthophoto produced with Trimble Business Center 

Photogrammetry module

IMAGE QUALITY & PERFORMANCE 

The quality of the deliverables is dependent on the quality 

of the photogrammetric equipment used. The innovative 

Trimble UX5 Aerial Imaging Rover has been designed to 

follow the latest developments in the ‘prosumer’ camera 

market, ensuring optimal image quality along with maximum 

photogrammetric accuracy. 

Trimble selected the Sony NEX-5R mirrorless camera because 

of its large APS-C (CMOS) sensor with 16.1 megapixel count. 

While the 1/1.7” sensor of the Ricoh GRD IV camera used in 

the Trimble Gatewing X100 was already 1.5 times larger than 

other compact cameras in the market, the surface area of the 

Sony NEX-5R sensor is nearly 9 times that of the Ricoh GRD 

IV. In addition to the significant increase in the pixel count, 

the size of each individual pixel with the Sony NEX-5R is more 

than 5x the Ricoh GRD IV pixels. This class-leading pixel size 

is important because it allows for a sharp increase in light 

In addition to producing these typical photogrammetric 

deliverables from Trimble Business Center, the aerial imagery 

data can be combined with Trimble VISION products such as 

the Trimble VISION total stations and Trimble 3D laser scanners 

for a one-of-a-kind solution in the market. Orthophotos are 

primarily used to create scaled images of a site that accurate 

WWW.TRIMBLE.COM/UAS 3

26
FIGURE 9 Sony NEX-5R camera and Voigtländer lens used in the 

Trimble UX5 Aerial Imaging Rover

sensitivity, dynamic range, and signal to noise ratio resulting 

in drastically reduced noise even at high ISO values. Combined 

with the much shorter ISO determination time of a system 

camera compared to a compact camera, it allows the user to 

use a fixed shutter speed and an automatically adjusted ISO 

ranging between 100 and 3200, yielding sharp, contrast rich 

images with a constant brightness, even in adverse and rapidly 

changing light conditions and shadow areas. This eliminates 

the need for users to judge brightness and manually set both 

the shutter speed and ISO to a fixed value throughout a flight. 

 From a photogrammetric perspective, the biggest advantage of 

the Trimble UX5 camera compared to using a compact camera 

in Aerial Imaging Rovers is the external lens. External lenses 

inherently offer a more stable internal geometry resulting in 

a more reliable camera calibration than that of a retractable 

lens. For the UX5, a light-weight 15 mm fixed focal length 

Voigtländer lens featuring mechanical focus and aperture ring, 

was chosen. To further increase the stability of the internal 

geometry, a custom adapter was designed by Trimble to replace 

the standard camera and lens mounts, which allow rotational 

movements of the principal point, by a two-part screw mount 

adapter. Additionally, the lens is fitted with a locking screw to 

fix the focus ring in the manufacturer-recommended position. 

This position is fixed using a collimator during production, 

ensuring not only sharp imagery across the flying height range 

(75 - 5000 m), but also a more stable focal length throughout 

all projects. The improved stability of the camera directly results 

in an increased accuracy of the deliverables, especially areas 

between the ground control points. 

Mounted in front of the APS-C sensor, the focal length 

expressed as 35mm-equivalent of the UX5 camera is 22.5mm, 

yielding a wide field of view. This means that, at a flying height 

of 150 m, the Trimble UX5 produces an image footprint of 235 

m by 157 m which is 40% larger than other UAS. Combining 

this field-of-view with the increased shutter speed, the Trimble 

UX5 has a larger overlap of the images than other systems, 

resulting in better accuracy of the DSM that is generated 

from the photos. The combination of these photogrammetric 

advancements means that the Trimble UX5 can cover 50-75% 

more area per flight hour than the X100 and most other UAS 

products at the same flying height. This translates to greatly 

enhanced work efficiency and reduced operational costs.

At a flying height of 150 m, the Trimble UX5 produces a GSD 

of 4.8 cm. In addition, the Trimble UX5 is capable of flying 

as low as 75 m above ground level (AGL) and producing a 

GSD of 2.4 cm. Flying at such a low height requires faster 

shutter speeds on the camera to prevent forward motion blur. 

The Sony NEX-5R camera used in the Trimble UX5 is capable 

of using the higher ISO values necessary to compensate the 

darkness resulting from the fast shutter speeds while keeping 

noise to acceptable levels for photogrammetric applications.

FIGURE 10 comparison X100 coverage and UX5 coverage

UX5 coverage

X100 coverage

WWW.TRIMBLE.COM/UAS 4

27
RELIABLE & RUGGED DESIGN

The new Trimble UX5 Aerial Imaging Rover builds on the 

standards set by its predecessor, the first commercial aerial 

imaging rover on the market, the Trimble Gatewing X100. 

Key features of the Trimble Gatewing X100 are also available 

in the Trimble UX5, such as all-weather flight capability, while 

surpassing its design of the airframe, making it a heavy-use, 

all-terrain device with the best accuracy and image quality 

available. 

FIGURE 11 UX5 top view

The Trimble UX5 Aerial Imaging Rover is based on a production 

method patented by Trimble. The base structure consists of a 

carbon frame inside expanded polypropylene foam. The frame 

ensures torsional stiffness and rigidity while the foam has 

exceptional pressure resistance and no memory-effect, which 

means that it will ‘bounce back’ to its original shape after 

impact. The exterior foam protects the internal electronics on 

impact and reduces the likeliness of any (physical) damage in 

case of an incident. 

The Trimble UX5 has a longer life expectancy than many other 

similar aircraft and is considered a wing suitable for heavy use. 

This new wing design produces a more rigid aircraft without 

compromising flight efficiency. Parts used in the motor 

assembly, the container for the flight electronics (also called 

‘eBox’) and servos are made of impact resistant plastics. The 

composite fiber parts of the elevons, the moving and fixed 

parts of the trailing edge of the wing, are light-weight and 

have an internal matrix structure that absorbs energy. The 

vertical winglets are made of a composite that allows bending 

in one direction to absorb energy during rough landings. 

Further, the Trimble UX5 belly plate is uniquely designed to 

absorb energy during landing as well as reduce abrasion from 

rough terrain such as rocks or tarmac.

FIGURE 12 UX5 bottom view

Due to its structural strength and additional energy absorption, 

maintaining the Trimble UX5 is easy. The Trimble UX5 offers 

operators a user-friendly design with replaceable parts such as 

vertical tails and propellers. The wing component is extremely 

durable and ideal for tough terrain. Some users will be able 

to work with just one airframe (or wing component) for 

years. This level of durability results in low yearly operation 

and maintenance costs of the Trimble UX5, which makes it a 

favorable system for the frequent (daily or weekly) use.

WWW.TRIMBLE.COM/UAS 5

28
ACCURATE LANDINGS

The Trimble UX5 starts its final landing phase at the a height 

above ground level (AGL) of 75 m only 200 m from the 

designated landing location. The touch down is, on average, 

within a 10 m (radius) circle of the designated location. Offsets 

that double this value are extremely rare. 

A traditional landing for an Aerial Imaging Rover has limitations 

that must be considered and addressed: the glide slope and 

landing speed. An efficient aircraft with good range and 

coverage has a disadvantage over an aircraft that consumes 

a lot of energy to stay aloft: the glide angle is rather small. A 

steeper approach would be means to reduce this offset but 

would result in a higher approach speed. 

75 m

ø 200 m

300 m

The Trimble UX5 has been engineered to overcome the 

limitations of a traditional landing with the addition of 

an advanced control method and improving the height 

measurement resulting in accurate and predictable landings. 

The advanced control method included in the Trimble UX5 is a 

thrust reversal on approach. During thrust reversal, the motor 

and propeller direction is reversed. This has the same effect as 

using a propeller with opposite pitch. By reversing the thrust, 

the propeller starts pulling air instead of pushing it. This gives 

the aircraft a means to counteract the speed increase that 

results with a steep descent. 

Thrust reversal (or also called ‘reversed thrust’) allows for an 

advanced control method that relies on changing the propeller 

from forward to reversed speed. This challenges aerodynamics, 

electronics and control algorithms. It challenges aerodynamics 

because applying a pulse of reversed thrust can result in stall 

effects of wing and elevons. It challenges electronics because 

FIGURE 13 Landing pattern UX5

having smooth control from forward to reverse is difficult for 

electronic speed controller (ESC). And it challenges control 

algorithms because it needs to cope with limits set by the 

aerodynamics and electronic speed controller and non-linear 

behavior because of asymmetry in the reversed and forward 

mode. A propeller that turns in reversed mode delivers thrust 

but also creates torque and aerodynamic effects that need to 

be monitored and controlled.

AUTOMATED CHECKS & IMPROVED WORKFLOWS 

The new Trimble Access Aerial Imaging application is a single 

software tool for planning Trimble missions, performing 

pre-flight checks and monitoring flights – all with intuitive 

workflows that ensure reliable results and safety of the 

individuals involved.

Trimble Access Aerial Imaging application offers mission 

planning that can be performed in the office or on the Ground 

Control Station (GCS). The project area and avoidance zones 

are drawn on top of an industry-standard map interface. The 

flight height above ground level (AGL), Ground Sample Distance 

(GSD) and photo overlap are defined and Trimble Access 

calculates the number of flights, flight pattern and duration 

of flight(s). The locations for takeoff and landing are proposed 

and then the project is taken to the field for the flight. 

FIGURE 14 Trimble AccessTM 

In the field, the operator is guided through the pre- and 

post-flight sequences with step-by-step digital checklists. 

Many of the Trimble UX5 checks are automatically verified 

by the software and sometimes run in the background (selfcheck routines) and do not require any interaction from the 

operator. This makes the setup process (before launch) and 

data recovery (after landing) easy and reliable. 

With these wizard-like digital checklists, it is impossible for the 

operator to forget or bypass a critical step, ensuring reliable 

and safe flights. The software also requires the operator to 

follow a fixed post-flight procedure for downloading the data 

and verifying the data. This safeguards that the user does not 

leave the field with a dataset that is incomplete or inconsistent. 

WWW.TRIMBLE.COM/UAS 6

29
Some examples of automated pre-flight checks are:

f battery connection and status

f ground control station connection and status

f aircraft parameter self-check (when arming the system)

f camera trigger check

f elevon response check

f sensor and gps checks

FIGURE 15 pre-flight check

CONCLUSION

The Trimble UX5 Aerial Imaging Solution sets a new standard 

in accuracy, robustness and performance for photogrammetric 

aerial mapping. The imaging performance of the Trimble 

UX5 Aerial Imaging Rover and the streamlined workflows of 

Trimble Business Center Photogrammetry application allow for 

the creation of professional deliverables with unprecedented 

accuracy and quality. Costs for data acquisition are drastically 

reduces when compared to collecting the same level of detail 

using traditional methods and technologies.

What was once reserved for large photogrammetry specialists 

is now available for a variety of geospatial applications. 

Trimble’s innovation in aerial photography can now be used 

to generate very detailed and useful deliverables by itself, 

however, by coupling UAS technology with other survey 

technologies such as GNSS, imaging total stations and 3D 

laser scanners, Trimble offers an unparalleled way to visualize 

and measure the world.

For more information visit trimble.com/uas

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UX5 HP UX5 faa exemption specifications user stories flight calculator

High Precision Mapping and Surveying

 Solution

The Trimble UX5 HP is a professional aerial mapping system,

 designed to capture the highest image accuracy for survey

 applications. The features of the new UX5 High Precision include an

 integrated Trimble GNSS receiver, a powerful new camera, and a

 selection of camera lenses available for the ultimate in system

 flexibility.

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UX5 HP

HIGH PRECISION

 FOR SUPERIOR

 DELIVERABLES

SELECT A

 CONFIGURATION

 THAT IS RIGHT

 FOR THE JOB

TIME SAVINGS IN

 THE FIELD

CAPTURE THE

 HIGHEST

 QUALITY DATA

 IN EXTREME

 TEMPERATURES

INTUITIVE FIELD

 TO OFFICE

 WORKFLOW

 SOLUTION

31
High Precision for Superior

 Deliverables 

The best geospatial deliverables require

 accurate and timely image and position

 data. The UX5 HP will lead the market in

 precise data by integrating a highperformance GNSS receiver and a new

 Sony a7R camera. The Sony a7R is an

 industry leading, full-frame sensor, 36MP

 high-resolution camera. The camera in

 addition to the GNSS receiver achieves a

 leading level of image accuracy

—orthomosaics resolution down to 1 cm and

 3D models with up to 1,000 pts/m2. Postprocessed kinematic (PPK) GNSS

 technology is used to establish image

 locations in absolute coordinate systems,

 minimizing, or even eliminating in some

 cases, the need for ground control and

 greatly increasing the value of the

 deliverable. This level of precision is ideal

 for power line modeling, field leveling and

 site planning.

Select A Configuration That

 Is Right For The Job 

No one project is ever the same. Now users

 can select a camera and lens combination

 that match project needs. Not only is there

 an option to choose between a near infrared

 or RGB sensor, now there is a selection of

 lenses available. The three new lenses

 include a 35mm lens for high accuracy, a

 15mm wide angle lens for increased flight

 coverage or a 25mm lens delivering both

 accuracy and increased flight coverage. No

 matter what a job requires, now there are

32
 options to meet the needs of diverse project

 requirements. 

Time Savings in the Field 

With the addition of an integrated, highperformance Trimble GNSS system and

 PPK to establish image locations, ground

 control points (GCP) are no longer

 required in the field. This not only saves

 time in placing GCP’s but also eliminates

 the risk associated with laying GCPs in

 often dangerous environments such as pit

 mines or dense vegetation.

Capture the highest quality

 data in extreme

 temperatures 

The Trimble UX5 HP is an extremely strong,

 durable system made from impact resistant

 foam that can withstand extreme

 temperatures, winds up to 55 km/h and light

 rain, making it ideal for use in conditions

 that many other unmanned aerial vehicles

 struggle to operate in.

33
Intuitive Field to Office

 Workflow Solution 

The Trimble Access Aerial Imaging

 application loaded onto the Trimble Tablet

 Rugged PC operates the UX5 HP and is a

 single software tool for planning your aerial

 missions, performing pre-flight checks and

 monitoring your flights. Optimized to

 process data from the Trimble UX5 HP, the

 Trimble Business Center Photogrammetry

 Module creates impressive deliverables.

 Specialized computer-vision algorithms

 produce a scaled orthophoto, point clouds,

 Triangulated Irregular Network (TIN) models

 and contour maps of the area flown

 automatically, with minimal manual

 interaction. Making it possible to process

 complete survey projects. (These can then

 be used in planning a project, calculating

 volumes, excavation planning, drainage

 planning and many other functions).

 Alternatively, Inpho UASMaster provides the

 power user or photogrammetrist with the

 right set of tools to use the full potential of

 aerial data.

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35
Trimble UX5 HP

Unmanned Aircraft System

HIGH PRECISION MAPPING 

AND SURVEYING SOLUTION

The Trimble® UX5 HP Unmanned Aircraft System 

(UAS) is an easy to use, fully automated, high 

precision system capable of capturing aerial 

photography with resolutions down to 1 cm. 

Featuring Trimble AccessTM Aerial Imaging field 

software and Trimble Business Center office 

software, this complete system provides an intuitive 

workflow that allows you to quickly create the 

highest quality orthomosaics and 3D models for 

applications such as survey grade mapping, power 

line monitoring, field leveling, site and route 

planning, progress monitoring and asset mapping. 

Superior Image Acquisition 

and Accuracy

The UX5 HP delivers precise data by integrating 

a high-performance Trimble GNSS receiver and 

a superior camera. Post-Processed Kinematic 

(PPK) GNSS technology is used to establish very 

accurate image locations in absolute coordinate 

systems, eliminating the need for ground control. 

As a result, less time is spent in the field and 

high precision results can be achieved even in the 

most inaccessible areas. With PPK, georeferencing 

aerial data is more robust and accurate than RTK, 

providing a superior level of reliability and accuracy. 

Use either your own base station or work with 

data from reference stations to georeference your 

deliverables with the highest accuracy possible.

The Trimble UX5 HP features an industry-leading 36 

MP full-frame sensor camera capable of capturing 

sharp, high resolution images. The camera achieves 

a leading level of image resolution—orthomosaics 

down to 1 cm GSD and point clouds up to several 

thousands points per square meter.

Key Features 

High-performance Trimble GNSS receiver 

with PPK technology

36MP, full-frame, high resolution camera

Orthomosaics resolution down to 1 cm & 

3D models with up to 1,000 pts/m2 

Survey quality accuracy without 

ground control 

Fully automated Trimble Access 

workfl ows for ease of-use and 

safe operation

Simple data processing with Trimble 

Business Center photogrammetry module 

Advanced data processing with Trimble 

Inpho UASMaster

DATASHEET

Configure for the Job 

No one project is ever the same, that is why you 

can select a camera and lens combination that 

match your project needs. You have the flexibility 

to choose between a near infrared or RGB sensor 

system, and a selection of lenses. The lenses 

include a 35mm lens for high accuracy, a 15mm 

wide angle lens for increased flight coverage or a 

25mm lens delivering both accuracy and increased 

flight coverage. 

Trusted Performance

The Trimble UX5 HP is an extremely safe and 

durable system, made from impact resistant foam, 

that can withstand extreme temperatures, winds up 

to 65 km, and light rain—making it ideal for use in 

conditions that most unmanned aircrafts struggle to 

operate in. 

Intuitive Workflows with 

Trimble Access

The Trimble Access Aerial Imaging application 

loaded onto the Trimble Tablet Rugged PC operates 

the UX5 HP and is a single software tool for 

planning your aerial missions, performing pre-flight 

checks and monitoring your flights. Now you can 

map corridors, cover disconnected areas in a single 

flight, import multiple map layers, fly irregular 

shaped areas and heights, plan or change multiple 

takeoff and landing locations during flight, and 

perform flight simulations to confirm the plan. 

The export functionality gathers all required data 

into a single file that can be imported into Trimble 

Business Center.

Valuable Photogrammetry Deliverables

Optimized to process data from the Trimble UX5 

HP, the Trimble Business Center Photogrammetry 

Module creates impressive deliverables. With a 

single drag-and-drop, imported GNSS information, 

base station or reference station data, and onboard 

images are processed in Trimble Business Center 

to produce a scaled orthophoto, point clouds, 

Triangulated Irregular Network (TIN) models and 

contour maps of the area flown. These can then 

be used in planning a project, calculating volumes, 

excavation planning, drainage planning and many 

other functions. 

Alternatively, Inpho UASMaster provides the power 

user or photogrammetrist with the right set of tools 

to use the full potential of aerial data. With featurebased seamline-finding, terrain editing capabilities, 

state-of-the-art DTM generation, classification and 

filtering, even the most challenging projects can 

be processed.

36
OPERATION

Endurance1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 40 minutes

Range1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 52 km (32 mi)

Cruise speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 85 kph (53 mph)

Maximum ceiling2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5000 m (16,404 ft)

Pre-flight system setup time . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 minutes

Take off

Type . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Catapult launch

Angle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 30 degrees

Landing

Type . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Belly landing

Angle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14 degrees

Landing space (L x W)3

Typical . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 m x 6 m (66 ft x 20 ft)

Recommended . . . . . . . . . . . . . . . . . . . . . . . . . . 50 m x 30 m (164 ft x 98 ft)

Weather limit . . . . . . . . . . . . . . . . . . . . . . . . . . . 55 km/h (34 mph) and light rain

Communication & control frequency . . . . . . . . . . . . . . . . . . . . . . 2.4 GHz (FHSS)

Communication & control range . . . . . . . . . . . . . . . . . . . . .Up to 5 km (3.10 mi)

ACQUISITION PERFORMANCE

Resolution (GSD) . . . . . . . . . . . . . . . . . . . . . . . . 1 cm to 25 cm (0.4 in to 9.9 in)

Height above take-off location (AGL) . . . . . . .75 m to 750 m (246 ft to 2,460 ft)

Absolute accuracy XY/Z (no ground control points) . . . . . . . . . down to 2 – 5 cm 

(0.8 – 2 in)

Relative orthomosaic/3D model accuracy . . . . . . . . . . . . . . . . . . .(1-2x/1-5x GSD)

AREA COVERAGE TABLE

Height 

AGL

GSD 

15 mm 

lens

Area/

flight 

15 mm 

lens

GSD

25 mm 

lens

Area/

flight 

25 mm 

lens

GSD

 35 mm 

lens

Area/

flight 35 

mm lens

75 m 

(246 ft)

2.4 cm

(0.9 in)

1.4 km2

(0.54 mi2

)

1.5 cm 

(0.6 in) 

0.8 km2 

(0.31 mi2)

1.0 cm 

(0.4 in)

0.6 km2

(0.23 mi2

)

100 m

(328 ft)

3.3 cm

(1.3 in)

1.9 km2

(0.73 mi2

)

1.9 cm 

(0.7 in)

1.2 km2

(0.46 mi2

)

1.4 cm 

(0.6 in)

0.8 km2

(0.31 mi2

)

120 m

(394 ft)

3.9 cm

(1.5 in)

2.4 km2

(0.93 mi2

)

2.3 cm 

(0.9 in) 

1.4 km2

(0.54 mi2

)

1.7 cm 

(0.7 in)

1.0 km2

(0.39 mi2

)

150 m

(492 ft)

4.9 cm

(1.9 in)

3.1 km2

(1.20 mi2

)

2.9 cm 

(1.1 in)

1.8 km2

(0.69 mi2

)

2.1 cm 

(0.8 in)

1.2 km2 

(0.46 mi2)

300 m

(984 ft)

9.8 cm

(3.9 in)

6.5 km2

(2.51 mi2

)

5.8 cm 

(2.3 in)

3.7 km2

(1.43 mi2

)

4.2 cm 

(1.7 in)

2.7 km2

(1.04 mi2

)

750 m

(2461 ft)

16 cm

(6.3 in)

16.1 km2

(6.22 mi2

)

14.6 cm 

(5.7 in)

9.3 km2

(3.60 mi2

)

10.5 cm 

(4.1 in)

6.3 km2

(2.43 mi2

)

1 For a 5:1 aspect ratio of a single rectangular flight block, at 80% lateral overlap, including 5 min of traveling time 

from take-off to the first waypoint and from the last waypoint to the landing.

PERFORMANCE SPECIFICATIONS

• Maximized image footprint without compromising resolution, obtained with 

a custom wide-angle lens and APSC-type sensor.

• Maximized coverage per flight and per hour due to large image footprint, 

sharp turning capability and high cruise speed.

• Reversed thrust technology for a short and steep landing circuit.

• Powerful propulsion system for steep climbs and high altitude flights.

• High airframe service life due to wing robustness and maintainability.

• Short setup time with automated procedures in Trimble Access field software.

• Self-check and failsafe procedures for safe operation.

• One-button export to Trimble Business Center to create deliverables.

• Optimized data accuracy when processed with Trimble Business Center or 

Trimble Inpho UASMaster.

• High Precision GNSS receiver to georeference deliverables accurately and 

easily.

HARDWARE

Type . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Fixed wing

Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.9 kg (6.4 lb)

Wingspan . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 m (3.3 ft)

Wing area . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 34 dm2

Dimensions . . . . . . . . . . . .100 cm x 65 cm X 10.5 cm (39.4 in x 25.6 in x 4.1 in)

Material . . . . . . . . . . . . EPP foam; Carbon frame structure; Composite elements

Propulsion . . . . . . . . . . . . . . . Electric pusher propeller; brushless 1400 W motor

Battery . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .14.8 V, 6600 mAh

Camera . . . . . . . 36 MP mirrorless full frame with custom 15, 25 or 35 mm lens

GNSS receiver . . . . . . . . . . . . . L1/L2 GNSS (GPS, Glonass, Beidou, Galileo Ready)

Controller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Trimble Tablet Rugged PC

SOFTWARE

Trimble Access Aerial Imaging application

• Project management

• Mission planning with option for multiple flights

• Automated pre-flight checks

• Automatic take off, flight and landing

• Autonomous camera triggering

• Automated fail-safe routines

• User controlled fail-safe commands

• Automated data consistency checks

• Export to Trimble Business Center, Trimble UASMaster and a generic format 

for image processing

Specifications subject to change without notice.

Trimble UX5 HP

Unmanned Aircraft System

DATASHEET

1 ISO standard atmosphere conditions.

2 Recommended; UX5-HP not tested above 5,000 m (16,404 ft).

3 1 sigma for wind <30 kph (19 mph).

© 2013–2015, Trimble Navigation Limited. All rights reserved. Trimble and the Globe & Triangle logo are trademarks of Trimble 

Navigation Limited, registered in the United States and in other countries. Access is a trademark of Trimble Navigation Limited. All 

other trademarks are the property of their respective owners. PN 022516-131A (06/15)

TRIMBLE AUTHORIZED DISTRIBUTION PARTNER

NORTH AMERICA

Trimble Navigation Limited

10368 Westmoor Dr

Westminster CO 80021

USA

EUROPE

Trimble Germany GmbH

Am Prime Parc 11

65479 Raunheim 

GERMANY

ASIA-PACIFIC

Trimble Navigation 

Singapore Pty Limited

80 Marine Parade Road

#22-06, Parkway Parade

Singapore 449269 

SINGAPORE

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UX5 HP UX5 faa exemption specifications user stories flight calculator

Specifications

Category Item UX5 UX5 HP

HARDWARE Type fixed wing fixed wing

Weight 2,5 kg (5.5 lb) 2,9 kg (6.4 lb)

Wingspan 100 cm (39.4 in) 100 cm (39.4 in)

Wing area 34 dm 34 dm

Dimensions

100 x 65 x 10.5 cm 

(39.4 x 26 x 4.1 in)

100 x 60 x 10.5 cm 

(39.4 x 23.6 x 4.1 in)

EPP foam; carbon frame

2 2

38
Material

EPP foam; carbon frame

 structure; 

composite elements

 structure;

Composite elements

Propulsion

electric pusher propeller; 

brushless 700 W motor

electric pusher propeller, 

brushless 1400 W motor

Battery 14.8 V, 6000 mAh 14.8 V, 6600 mAh

Camera 24 MP mirrorless APSC

36 MP mirrorless full frame with

 custom

15, 25 or 35 mm lens

SOFTWARE Project management √ √

Mission planning multiple flights multiple flight

Automated pre-flight checks √ √

Automatic take off, flight and

 landing

√ √

Autonomous camera triggering √ √

Automated fail-safe routines √ √

User controlled fail-safe

 commands

√ √

Automated post-flight checks √ √

Trimble AccessTM integration √ √

OPERATION Endurance 50 min 40 min

Range 60 km (37 mi) 52 km (32 mi)

Cruise speed 80 km/h (50 mph) 85 km/h (53 mph)

Maximum ceiling 5000 m (16,404 ft) 5000 m (16,404 ft)

Pre-flight setup time 5 min 5 min

1

1

2

39
Take off type catapult launch catapult launch

Take off angle 30 deg 30 deg

Landing type belly landing belly landing

Landing angle 14 deg 14 deg

Typical landing spacing (L x

 W)

20 x 6 m (66 x 20 ft) 20x 6 m (66 x 20 ft)

Recommended landing spacing

 (L x W)

50 x 30 m (164 x 98 ft) 50 x 30 m (164 x 98 ft)

Weather limit 65 km/h (40 mph) & light rain 55 km/h (34 mph) & light rain

Communication & control

 frequency

2.4 GHz 2.4 GHz

Communication & control range up to 5 km (3.1 mi) up to 5 km (3.1 mi)

ACQUISITION

PERFORMANCE

Resolution (GSD) 2.0 - 19.5 cm (0.79 - 7.6 in) 1.0 - 25 cm (0.4 - 9.9 in)

Height above take off location

 (AGL)

75 - 750 m (246 - 2,460 ft) 75 - 750 m (246 - 2,460 ft)

Coverage check with flight calculator check with flight calculator

ISO standard atmosphere conditions

UX5/UX5 HP: recommended, not tested above 5,000 m (16,404ft)

1 sigma for wind < 30 kmh (19 mph)

3

1 

2

3

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41