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    Project Delivery Methodology (PDM)

    System Requirements

    Carleton University

    UNMANNED AERIAL VEHICLE FOR

    FARM CROP SURVEILLANCE

    VERSION: 1.1 REVISION DATE: 10 OCT 2014

    Approval of the System Requirements indicates an understanding of the purpose and content described

    in this deliverable. By signing this deliverable, each individual agrees with the content contained in thisdeliverable.

    Approver Name Title SignatureDate

    Prof. Artemev

    Prof. Tan

    Prof. Nitzshe

    Mr. Bauer

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    Unmanned Aerial Vehicle for Farm Crop Surveillance System RequirementsVersion 1 October 6, 2014

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    System Requirement Document. V 1.1 | 6 OCT 2014 Page 2 of 9

    Contents

    Section 1 Purpose ........................................................................................................................................ 3

    1.2 Acronyms ............................................................................................................................................ 3

    Section 2 General System Requirements .................................................................................................... 3

    2.1 Major System Capabilities ............................................................................................................. 3

    2.2 Major System Conditions .............................................................................................................. 4

    2.3 System Interfaces .......................................................................................................................... 4

    2.4 System User Characteristics .......................................................................................................... 4

    2.5 General Constraints ...................................................................................................................... 5

    2.6 System Requirements ................................................................................................................... 5

    Section 3 Policy and Regulation Requirements .......................................................................................... 7

    3.1 Policy Requirements ..................................................................................................................... 8

    3.2 Regulation Requirements ............................................................................................................. 8

    Section 4 Security Requirements ................................................................................................................ 8

    Section 5 Training Requirements ................................................................................................................ 8

    Section 6 References ................................................................................................................................... 8

    Section 7 Document Revision History ......................................................................................................... 9

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    Section 1 Purpose

    The purpose of the System Requirements document is to specify the overall system requirements that

    will govern the development and implementation of the 2014 MAAE 4907 fixed-wing UAV project. The

    document will outline initial system requirements, security, and training agreed upon by the project

    sponsor and key stakeholders. The SRD is iterative, and new versions are to be added.

    1 2 Acronyms

    AGL above ground level

    AME aircraft maintenance engineer

    ASL above sea level

    FAA Federal Aviation Administration

    FOM Figure of Merit

    GCS ground control station

    SRD system requirements document

    TBD to be determined

    TBR To be reviewed

    TBO time between overhaul

    TC Transport Canada

    UAV Uninhabited aerial vehicle

    CAR Canadian Aviation Regulations

    AWM Airworthiness Manual

    Section 2 General System Requirements

    2 1 Major System Capabilities

    - The fixed-wing UAV will provide crop surveillance for farms and gather data on crop

    health, land topography, pests, etc (aspects of interest to a farm operator to ensure

    smooth operation of a farm).

    - The system shall be readily available and easy to deploy.

    - The system shall be deployable from any farm.

    - The UAV shall be capable of flying without the need for a trained pilot to control it.

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    - The system shall have a health monitoring system which will detect structural

    damage that may make the flight unsafe and will return the UAV to base or execute a

    forced landing. [TBR]

    2 2 Major System Conditions

    - The system is targeted for agricultural farms.

    - The system shall run on readily available fuel.

    - The UAV will be subject to weather limitations [TBD].

    - The system shall be deployable by any user without a trained pilot.

    2 3 System Interfaces

    The UAV system shall be automated to enable autonomous takeoff, flight, data acquisition, and landing.

    The flight plan shall be uploaded to the UAV by the user. The UAV shall then be deployed in the location

    of interest and begin its autonomous flight. After completing the surveying mission, the UAV will self-

    land to allow the user to efficiently upload the data of interest.

    The UAV shall have a recovery system that will either return the UAV to base or execute an emergency

    landing if flying conditions deteriorate or if any structural damage occurs that renders flying unsafe.

    The user shall not be required to participate in the actual flying of the UAV: flight will be fully

    autonomous. The user shall interact with the system during flight programming, uploading flight

    programs, deploying the UAV, recovering the UAV, receiving flight and surveillance data, and

    maintaining the UAV and its systems.

    The UAV shall provide thermal and multispectral vision using the proposed payload.

    The UAV shall be able to provide live data to the user.

    The UAV shall be handled by a minimum of two persons at all times.

    2 4 System User Characteristics

    The system is to be used by crop consultants. The system uses the availability of gravel roads

    and grass fields in farms for takeoff and landing. The user deploys the UAV system to inspect a field. The

    system can be deployed in any location with ground elevation of 5000 ft ASL. The user shall be able to

    program the flight path and layout survey lines for the farm.

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    2 5 General Constraints

    2 6 System Requirements

    Tag Criteria Threshold

    Requirement

    Objective

    Requirement

    Rationale Status

    001 Range 12.5 miles TBD Based on number

    and length of passes

    to cover a field and

    return to base.

    TBR

    Subject t

    o

    increase

    002 Endurance 60 minutes 90 minutes Covering a field at

    minimum cruise

    speed will take

    approximately 60

    minutes. An

    allowance of 30

    minutes was

    included.

    TBR

    Subject

    to

    increase

    Requirement Rationale Cert.

    Status

    Status

    Minor UAV service should be

    able to be performed by

    operator(s) on site. Using

    simple hand tools such asscrew drivers

    This avoids the cost of transporting

    the UAV for minor services. This may

    include routine engine replacement.

    TBD

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    System Requirement Document. V 1.1 | 6 OCT 2014 Page 6 of 9

    003 MTOW 55 lb 44 lb For certification

    purposes: any aerial

    vehicle above 55 lb

    requires a trained

    pilot [CARs].

    Secondary rationale

    is for ease of

    transport.

    TBR

    004.a Cruise speed

    (indicated)

    31 mph

    [28 kts]

    40.5 mph

    [36 kts]

    Lower cruise speeds

    allow for better

    imaging quality.

    TBR

    004.b Minimum speed TBD

    004.c Maximum speed 43.5 mph

    [39 kts]

    56 mph

    [50.5 kts]

    005 Transport 96 in long x 50 in wide x 36 in high Must be easily

    transportable to/from

    operating area in a

    conventional road vehicle.

    This is the typical box size

    of a full size pickup truck.

    FIXED

    005.a The entire UAV

    operational

    system shall be

    able to fit within a

    005.b The complete

    UAV operational

    system shall be

    able to fit within

    an Air Canada

    cargo container

    7.16 ft long x 10.25 ft wide 5.25 ft

    high

    Allows for economic means

    of transportation by a

    conventional transport

    means.

    006 Automatedtakeoff and

    landing

    Takeoff and land in the presenceof crosswinds while maintaining

    ground communication and

    flight position

    This will allow easeof use by farmers

    (or laymen in

    general) via

    automation.

    TBR

    007 Absolute ceiling

    (ASL)

    7000 ft 6500 ft This is based on the

    average ground elevation

    of farms in Canada.

    FIXED

    008 Surveillance

    altitude (AGL)

    400 ft 390 ft This takes into

    account the

    altitude that

    sensors need to beat for scanning a

    field.

    400 ft (AGL) is the

    limit of where

    clearance is needed

    [FAA]

    TBR

    009 Takeoff roll (if 300 ft 200 ft Based on the length of an TBR

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    System Requirement Document. V 1.1 | 6 OCT 2014 Page 7 of 9

    conventional) average sized field in the

    Experimental Farm

    (Ottawa)

    010 Maximum landing

    Roll

    300 ft 200 ft TBR

    011 Obstacle

    clearance (end ofrunway)

    Landing and

    Takeoff

    8 ft 10 ft Based on the height of the

    highest crop produced(corn)

    TBR

    012 Runway condition Grass fields and gravel roads Allows for takeoff from any

    unprepared runways in a

    farm.

    FIXED

    013 Payload 6.6 lb 5.5 lb This includes mission and

    flight avionics payloads.

    TBR

    014 Communicationrange with ground

    1.5 mi 2.3 mi Based on diagonal distanceof two rectangular fields

    plus a safety margin.

    TBR

    015.a Fuel type The fuel used shall be readily

    available in a farm such as gasoline

    or diesel.

    This makes the UAV ready

    to operate at any time with

    fuel readily available /

    avoids the need for

    specialty fuel (which may

    be hard to come by,

    expensive, or both).

    TBD

    015.b The UAV shall not use battery

    power to provide power for

    propulsion.

    This eliminates the time

    needed to recharge

    batteries. Battery power is

    also avoided for weight

    reduction.

    FIXED

    016 Climb rate TBD

    017 Payload

    installation

    TBD

    018 Cost TBD

    019 Assembling The user shall be able to assemble

    the UAV with readily available

    simple hand tools

    It should not require more

    than 2 persons to assemble

    it.

    Section 3 Policy and Regulation Requirements

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    System Requirement Document. V 1.1 | 6 OCT 2014 Page 8 of 9

    - The UAV shall comply with all laws and regulations outlined in CAR1 and AWM

    2.

    - Flight clearance is needed for any flight above 400 ft AGL which may limit the

    mission performance if flight clearance is to be avoided.

    - CARs requires that any aerial vehicle above 55 lb requires a trained pilot to operate

    it; therefore, 55 lb is the maximum threshold.

    3 1 Policy Requirements

    TBD

    3 2 Regulation Requirements

    TBD

    Section 4 Security Requirements

    TBD

    Section 5 Training Requirements

    The system shall not require the user to undergo training to fly the UAV. The user interface shall

    be simple and user-friendly, such that only a familiarization session shall be sufficient for any user

    to easily learn to fully operate the UAV.

    The user shall not be engaged in flying the UAV. The users responsibility shall only be to upload

    the mission and flight data to the system, deploys the UAV and then recover it and upload the

    collected data.

    The training/tutorial shall cover all aspects of the UAV system including system familiarization,

    flight programming and interface, operation, deployment, recovery, and maintenance.

    Section 6 References

    Document No. Document Title Date Author

    1CAR 623.65(d) Unmanned Air Vehicle

    2Transport CanadaAir Worthiness Manual Chapter 525

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    System Requirement Document. V 1.1 | 6 OCT 2014 Page 9 of 9

    Section 7 Document Revision History

    Version Date Name Description

    1.0 6 OCT 2014 Integration Team (INT)Y. Berestetsky

    A. Jabakhanji

    B. The

    J. Gill

    M. Youn

    K. Adem

    Initial SystemRequirements

    Document

    [initial creation]

    1.1 10 OCT 2014 Integration Team -Updated values

    -Added requirements