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JOUAV CW-15 Manual

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C
W-15UAVMANUAL

Version1.1   March,2023




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Summary of Contents for JOUAV CW-15

  • Page 1 W-15UAVMANUAL Version1.1   March,2023...
  • Page 2 RevisionRecord  VersionNo.  RevisionContent  Reviser  Date  Finalizedthefirstversionforoutward August30, V1.0  MaoCen distribution  2022  March8， V1.1  2022...

  • Page 3: Foreword

    ALLRIGHTRESERVED © 2021-CHENGDUJOUAVFUSIONTECHCO.,LTD. WithoutthewrittenconsentoftheCompany,nounitorindividualshallmake commercialapplicationandcommercialcommunicationofpartorwholeofthe Manualinanyformsuchasexcerptandreproduction. Trademarks JOUAV is an important intellectual property right of CHENGDU JOUAV FUSIONTECHCO.,LTD.(hereinafterreferredtoasJOUAVLtd.).CHENGDUJOUAV FUSION TECH CO.,LTD. is a wholly-owned subsidiary of JOUAV Ltd. which is authorizedtousetherelevantintellectualpropertyrightsofJOUAVLtd.  Attention: TheManualisonlyusedasapplicableguidance.Theseriesofproductsand servicesyoupurchasedarespecificallyboundbythecommercialcontractsand termsofCHENGDUJOUAV ® FUSIONTECHCO.,LTD.ThecontentsoftheManual donotconstituteanyformofstatement,guaranteeorwarrant. Disclaimer JOUAV ®...
  • Page 4 ALL RIGHT RESERVED © CHENGDU JOUAV FUSION TECH CO.,LTD SafetyPrecautions Thisproductisakindofspecialcontrolitem,whichcanonlybeusedsafely after being familiar with it for a period of time and can onlybe operated after gainingcertainprofessionalknowledge.Incorrectoperationmaycauseproduct damage,propertyloss,personalinjuryorevendeath,thustheoperatorshallbear correspondingresponsibilities.Inordertobetterusethisequipmentandensure yoursafety,pleasereadtherelevantmanualcarefullyorconsultthemanufacturer before use. Do not use unofficially provided or recommended parts. Official guidanceshallbefollowedfortheoperationanduseofthisproduct....
  • Page 5 MANUAL VersionInformation This Manual is applicable to the CW-15 DA PENG UAV. CHENGDU JOUAV FUSION TECH CO.,LTD reserves all the rights of the final interpretation of this document and all the documents related to this product. When there is any...
  • Page 6 ALL RIGHT RESERVED © CHENGDU JOUAV FUSION TECH CO.,LTD unified way, without separation notification. Please visit our official site, www. jouav.comtoacquirethelatestinformationaboutourproducts. Prohibitions Tips Reminder Annotation CW-15 UAV MANUAL PART 1...

  • Page 7: Table Of Contents

    ALL RIGHT RESERVED © CHENGDU JOUAV FUSION TECH CO.,LTD Contents  Foreword.....................1 PART1StandardOperationFlow..........6 1.SystemIntroduction..................7 FunctionalCharacteristics.................8 Performance ......................11 ListofArticles ......................12 2.OperationFlow......................13 Preparations ......................14 Check ........................15 Takeoff ........................16 Mission ........................17 Landing ........................19 EndofMission .....................21 PART2UAV....................1...

  • Page 8: Part1StandardOperationFlow

    ALL RIGHT RESERVED © CHENGDU JOUAV FUSION TECH CO.,LTD PART1Standard OperationFlow 1. SystemIntroduction 2. OperationFlow CW-15 UAV MANUAL PART 1...

  • Page 9: SystemIntroduction

    ALL RIGHT RESERVED © CHENGDU JOUAV FUSION TECH CO.,LTD 1.SystemIntroduction CW-15 UAV MANUAL PART 1...

  • Page 10: FunctionalCharacteristics

    ActiveSafetyTechnologyduringFlight Ground-imitationflightbasedonhigh-precisiondigital3Dmap  TheCW-15UAVsupportsthegroundimitationflightbasedonhigh-accuracy digital 3D map. With this function, CW-15 can adapt to more terrains, automatically generate height variable routes as per the surveying area and maintainaconsistentgroundresolutiontorealizebetterdataeffects. Aviation-classReliability Multi-sensorredundancytechnology  IMU, GNSS and barometer and other important sensors are redundantly backedup,andeachnodehaserrormanagementcapabilityaswellasautomatic recoveryandupdatecapability....
  • Page 11 UsabilityUpgradeofFixedWingUAV Automatedpreflightcheck  Thanks to the brand new avionics system and the online inspection of distributed avionics system networking of CW-15, the UAV can complete all preflightcheckitemsatthegroundbasestationbypressingonebutton,freeof complextraditionalflightinspectionsteps. Magneticcompassin-flightcalibration  This function is used to replace the ground calibration process of the magneticcompass,whichcanbecalibratedautomaticallybytheaircraftinflight basedontheGPSheading....
  • Page 12 ALL RIGHT RESERVED © CHENGDU JOUAV FUSION TECH CO.,LTD Heatingdrainpitot  The CW-15 UAV is equipped with a heating drain pitot to guarantee safe flightinplateaus,highhumidity,lowtemperatureandlightrain. SmartBattery  TheCW-15UAVisequippedwiththelatestCB100Sseriessmartbatteriesand correspondingsmartchargers.Inadditiontothehealthmanagementsystem,the smart batteries support the self-heating function that automatically enables at lowtemperaturetoguaranteeflightsafety. Ultra-highwaterproofness ...

  • Page 13: Performance

    ALL RIGHT RESERVED © CHENGDU JOUAV FUSION TECH CO.,LTD summaryandquery,etc.Itiscapableofactiveservicepushnotifications. Performance BasicPerformanceParameters Indexitems Indexes Remarks MTOW 17kg Minimumcruising Indicatedairspeed(sea 58km/h(16m/s) airspeed level) Economiccruise Indicatedairspeed(sea 61.2km/h(17m/s) airspeed level) Maximumcruising Indicatedairspeed(sea 110km/h(31m/s) airspeed level) Undertheconditionof Flightduration 120min cruisingaltitudeof1000m abovesealevel Undertheconditionof Endurancemileage 120km...

  • Page 14: ListOfArticles

    ALL RIGHT RESERVED © CHENGDU JOUAV FUSION TECH CO.,LTD ListofArticles ArticlesinsidePackingCase A total of 6 items are included in the packing case cover and central wing layer:1Verticaltail    2Horizontaltail    3Centralwing    4Receiverantenna    52.4Ggluestickantenna  6Whipantenna...

  • Page 15: OperationFlow

    ALL RIGHT RESERVED © CHENGDU JOUAV FUSION TECH CO.,LTD 2.OperationFlow CW-15 UAV MANUAL PART 1...

  • Page 16: Preparations

    ALL RIGHT RESERVED © CHENGDU JOUAV FUSION TECH CO.,LTD Preparations MissionPlanning The takeoff and landing routes and mission routes shall be planned in advance.Fordetails,seethesoftwareusesection. Amongwhich,whenplanningthetakeoffandlandingroute,thetakeoffand landingareashallbesuretobeflat,stableandfreeofobstacles,andtheaircraft will not pass over the heads of people when taking off and landing along the route. The whole route for takeoff and landing shall not pass over any tall...

  • Page 17: Check

    ALL RIGHT RESERVED © CHENGDU JOUAV FUSION TECH CO.,LTD 5. Removethefront-pullparts,firstinserttheconnectorintothesocketat thefrontendofthecentralwing,thenpressthelockingspringpin,andatthe sametime,insertthecarbontubeintothefrontendofthecentralwinguntilthe springpinpopsout. 6. Pushthesmartbatteryintothebatterybayuntilitislockedbythelocks onbothsides. Forassemblydiagrams,pleaserefertotheUAVoperationflow Check CheckafterAirframeAssembly Airframe part: The fuselage and wing surface are free from damage or deformation,wingandhorizontaltailscrewholesareperfect,allbaycoversand hinges are not damaged, and screws on the servo and pull rod shall be tight withoutlooseness....

  • Page 18: Takeoff

    ALL RIGHT RESERVED © CHENGDU JOUAV FUSION TECH CO.,LTD transmittedtotheaircraftuplink(requestparameteroperation)atthesametime. Remote control status: Check the remote control status of the commander softwareforwhetheritisinattitudemode. Sensor self-check: Check whether the sensor self-check information of the commander software passes correctly. If it fails, leave it to stand for another minute,orrestartthepoweroftheUAV....

  • Page 19: Mission

    ALL RIGHT RESERVED © CHENGDU JOUAV FUSION TECH CO.,LTD landonsite.Whenthevoltageofthepowerbatteryisfoundtobetoolow,and the power cannot ensure safety under the current environment by human judgment, the "Abort" command can also be used to land the aircraft immediately. Airspeed:Duringrotorclimbing,theairspeedshallberoughlyequaltothe current windward wind speed and relatively stable; if the airspeed is high (for example, it is greater than 10m/s, and the environmental wind is low) and continues to increase, the "Abort" command can be used to land the aircraft...
  • Page 20 UAVshallbegenerallywithin2m/s~6m/s.Iftheverticalvelocityiskeptnear0or negative during the climbing, excluding that the theoretical climbing limit is reached,itiscausedbyinsufficientpower,andtheaircraftshallreturnandland immediately. When the aircraft is flying horizontally, the vertical velocity shall fluctuatearound0. Airspeed: For CW-15 standard version, the indicated cruising airspeed is 17m/s,andtheindicatedclimbingairspeedis15m/s.Theairspeedvalueduring flightshallbebasicallyconsistentwiththeairspeedcorrespondingtothecurrent flightstatus. Theairspeedsetintheautopilotiscalculatedbasedonthesealevelandstandard atmospheric pressure (indicated airspeed/IAS); the higher the actual flight altitude, the thinner the air, and the higher the speed required to provide the sameliftforce.Theautopilotwillcalculatetheheightandchangethecommand...

  • Page 21: Landing

    ALL RIGHT RESERVED © CHENGDU JOUAV FUSION TECH CO.,LTD numberofsatellitesis0,theGNSSiscompletelylost,andtheaircraftshallreturn immediately. SafetyWarning During flight, if the backup GNSS has been enabled, the differential positioningcannotbeperformed.Notethattheremaybealargedeviationfrom thelandingpoint. Power: When the power supply is lower than 12V, the UAV shall return immediately.(Whentheautopilotbatteryislowerthantheflightreturnvoltage valueformorethan10s,itwilltriggerlowbatteryreturnandautomaticallyreturn to0point) Attitude: Normally, the UAV's maximum roll angle shall be 25°, and the...
  • Page 22 ALL RIGHT RESERVED © CHENGDU JOUAV FUSION TECH CO.,LTD normal"andthethrottlecommandis50%. Then, they shall re-confirm the landing direction is against the wind, the landing route is safe, and the status of the positioning GNSS is NARROWINT_RTK:1.0orNARROWINT:1.0. In case of wind direction change before landing, you may hold Shift and left-clicktodragthewaypoint797torotatethewholelandingroute. ...

  • Page 23: EndOfMission

    Blade:Checkandmakesurethatthereisnoobviousdamagetotheblade; use a wrench to manually tighten the blade to prevent it from loosening after operation.. Roll-upandPacking 1. Aircraftroll-upandpacking The roll-up and packing of the CW-15 UAV can be referred to the UAV operationflow. 2. Roll-upandpackingofgroundequipment (1) Roll-upofcontrolterminal Turnoffthepowersupplyofthecontrolterminal,disconnectthepowerline, closethecoverofthecontrolterminalandlockthepin....
  • Page 24 ALL RIGHT RESERVED © CHENGDU JOUAV FUSION TECH CO.,LTD Roll-upandpackingofgroundequipment The roll-up and packing of the ground base station can be referred to the operationflowinPART3. Turn off the power supply of the control terminal, disconnect the power line, closethecoverofthecontrolterminalandlockthepin. Fortheroll-upofsupportingequipment,pleaserefertotheoperationflowof thesupportingsystemtohavethetripodsandaccessorycasestored....

  • Page 25: Part2Uav

    PART2UAV Introduction Use Maintenance CW-15 UAV MANUAL PART 6...

  • Page 26: Introduction

    ALL RIGHT RESERVED © CHENGDU JOUAV FUSION TECH CO.,LTD 1.Introduction CW-15 UAV MANUAL PART 6...

  • Page 27: FunctionsAndPerformances

    The front pull power system provides the power required for flight of the fixedwing. The aircraft assembly can be disassembled into fuselage, central wing, left/right outer wing, left/right front rotor arm, left/right rear rotor arm, horizontaltail,front-pullparts,verticaltailandsoon. InterfaceSpecification ElectricalInterface TheCW15missionbayreservesthemissionequipmentinterfaceanddata downloadinterface.  CW-15 UAV MANUAL PART 6...

  • Page 28: Use

    ALL RIGHT RESERVED © CHENGDU JOUAV FUSION TECH CO.,LTD 2.Use CW-15 UAV MANUAL PART 6...

  • Page 29: UavDeployment

    UAVDeployment 1.CentralWingAssembly Removethedustcoveronthecentralwingandthemissionbay,andconfirm thatthelockinghandleofthemissionbayisintheopenposition. Inserttheconnectorontheabdomenofthecentralwingintotheconnector ontheupperpartofthemissionbayandslideitbacksothatthetriangulararrow slidesfromthehollowcircletotheblacksolidcircle,andthelockinghandle automaticallylocks. SafetyWarning Becarefulnottopinchyourhandsorfingersontherotorarmwhenfolding theaircraftforstorage. CW-15 UAV MANUAL PART 6...
  • Page 30 ALL RIGHT RESERVED © CHENGDU JOUAV FUSION TECH CO.,LTD 2.RotorArmDeployment Holdtherootoftherotorarmandpushitdowntothebottomoftherotating hinge,turntherotorarmuntiltheconnectorfits,andliftitup,thentheknobwill automaticallyturntothelockingposition.Deploytheremainingrotorarmsinthe sameway. Pleaseholdattherootoftherotorarmduringoperationtoavoiddamageto therotorarmhinge. CW-15 UAV MANUAL PART 6...
  • Page 31 3.OuterWingAssembly Insertthesquareandroundcarbontubesoftheleftouterwingintothe correspondingmatingholesontheleftsideofthecentralwing,andcompletethe insertionoftheconnectorsatthesametime; Connectthehaspontheleftouterwingandthecentralwingandthenlockit. Assembletherightouterwinginthesameway. SafetyWarning Preventtheairframefrombumpingandgettingdamagedduetoimbalance betweentheleftandrightsideswhenassembling/disassemblingtheouter wings. Preventtheconnectorcablefrombeingdamagedbypullingwhen disassemblingtheouterwings. Notethatthecooperationbetweenthearmandthecentralwingfollowsthe markingruleof"redontheleftandgreenontheright"! CW-15 UAV MANUAL PART 6...
  • Page 32 ALL RIGHT RESERVED © CHENGDU JOUAV FUSION TECH CO.,LTD 4.VerticalTailAssembly Inserttheplugatthefrontendoftheverticaltailintothesocketatthetailof thecentralwing,andtheninsertthecarbontubeintothefixingseatatthetailof thecentralwing.Rotatethehandlesonbothsidesuntiltheverticaltailcarbon tubeislocked. Insertthehorizontaltailintotheendoftheverticaltailandtightenthe thumbscrew.   SafetyWarning Please ensure that the horizontal tail is fully insertedandthethumbscrewistightened;otherwise, the flightsafetywillbeaffected. 5.AssemblyofFrontPullMotorPart  CW-15 UAV MANUAL PART 6...
  • Page 33 Firstinserttheconnectorintothesocketatthefrontendofthecentralwing, thenpressthelockingspringpin,andatthesametime,insertthecarbontube intothefrontendofthecentralwinguntilthespringpinpopsout. SafetyWarning Pleasemakesurethattheconnectorisfullyinserted, andtheupperandlowerendsofthespringpinare ejected;otherwise,theflightsafetywillbeaffected. 6.BatteryAssembly Pushthesmartbatteryintothebatterybayuntilitislockedbythelockson bothsides. CW-15 UAV MANUAL PART 6...

  • Page 34: UavRoll

    ALL RIGHT RESERVED © CHENGDU JOUAV FUSION TECH CO.,LTD SafetyWarning Theaircraftwillbepoweredonafterthesmartbatteryisassembled. Aftertheaircraftispoweredon,donotunplug/insertcomponentssuchas wingsandtailpipes,otherwisethecorrespondingCANequipmentmaybe damaged! UAVRoll-up 1. Openthebatterycompartmentcover,andpullthebatterystrapstoboth sides of the battery compartment to take out the smart battery and store it properlytopreventitfrombumping. 2. Accordingtothereverseoperationofdeployment,removethefront-pull parts,verticaltailandhorizontaltail,leftandrightouterwingsinturn,foldthe rotorarmsandunlockthecentralwingandthebridgewingofthefuselage. 3. Removethegroundbasestationandprepareforpacking. CW-15 UAV MANUAL PART 6...

  • Page 35: Maintenance

    3.Maintenance CW-15 UAV MANUAL PART 6...

  • Page 36: AirframeMaintenance

    ALL RIGHT RESERVED © CHENGDU JOUAV FUSION TECH CO.,LTD AirframeMaintenance Aftereveryflight,itisrequiredtocleanthefuselagetokeeptheairframefree ofstainsandresidualforeignmatterssoastoprotecttheaircraftfromchemical corrosion. After each flight and during general storage, the pitot shall be covered by pitotcovertopreventforeignmattersfromentering. Attheendofeachflightandduringnormalstorage,itisnecessarytocover therotorpropellerwithpropellerprotectionsleevestoavoiddamage. The aircraft shall be stored in a dry environment to avoid the adverse influencesofhumidityonthemeasurementaccuracyofautopilotsensors....
  • Page 37 . This transmitter must not be co‐located or operating in conjunction with any other antenna or transmitter. This equipment should be installed and operated with minimum distance 20cm between the radiator& your body. CW-15 UAV MANUAL PART 6...

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