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User Manual | Users Manual | 2.43 MiB | August 11 2020 | |||
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Int Photos | Internal Photos | 585.09 KiB | August 11 2020 | |||
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Ext Photos | External Photos | 4.11 MiB | August 11 2020 | |||
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FCC ID Label | ID Label/Location Info | 630.22 KiB | August 11 2020 | |||
1 2 | Block Diagram | Block Diagram | August 11 2020 | confidential | ||||
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Confidentiality Letter | Cover Letter(s) | 86.49 KiB | August 11 2020 | |||
1 2 | Operation Description | Operational Description | August 11 2020 | confidential | ||||
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Power of Attorney Letter | Cover Letter(s) | 64.61 KiB | August 11 2020 | |||
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RF Exposure | RF Exposure Info | 80.22 KiB | August 11 2020 | |||
1 2 | Schematics | Schematics | August 11 2020 | confidential | ||||
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Setup Photos | Test Setup Photos | 102.78 KiB | August 11 2020 | |||
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Test Report (Conducted) | Test Report | 1000.75 KiB | August 11 2020 | |||
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Test Report XOR (Radiated) | Test Report | 692.96 KiB | August 11 2020 |
1 2 | User Manual | Users Manual | 2.43 MiB | August 11 2020 |
CW S Instr Nov. 2019 9 Version 2
.0 Serie ructio s UAV on Ma V CW W-007 anual l 7 II Re eading T Tips Notation n Forbidde enWarnin ng Prom mpt Notes Technic al Suppo ort Webwww w.jouav.com m Tel+86-1 1838133837 73 Manuals s List CW-007 II Instructio on Manual CWCom mmander Ma anual CW-007 II Normal C Checklist CW-007 II Abnorma al Checklist t CW-007 II Emergen ncy Checkli ist CW-007 II Maintena ance Manua al Radio Co ontroller Ma anual Charger Manual checklist. Those are a all manuals we provide e for custom mers. The cu ustomers cann learn fromm manual an nd check by y C opyrightJOUA AV 1 1 Safety Regulation This is a special product, incorrect operation can cause harm resulting in bodily and/or death, user would be responsible for that. Must read manuals for safe and better using, or contact the manufacturer. Warning Attention Airspace Regulation This is Forbidden the law. Crew The mission should be allowed by local department who charge the airspace. Take off and land where is close to airport, railway, factory, electric tower, high voltage line, military installation, city and town, and the no-fly zone by the local government, department, and If the planned flight area has important protective targets or unclear targets, it shall be reported to the local police area for approval in addition to air traffic control. Flight Range Make sure that the airway is clear. There is turbulence in the buildings and mountains, do not fly in there. Each crew member should be trained by manufacturer and get the certification. Operate the system by procedure and checklist. The crew shouldnt feel tired and uncomfortable. Do not drink before flight. CopyrightJOUAV 2 Disclaimer JOUAV will not be responsible for the things as below. Forbidden Change the air-frame and payload without permission of manufacturer. Replace equipment and accessories with different models. Change the parameters of autopilot without permission of manufacturer. Change the ground control station. The crew member who was not trained by manufacturer or didnt pass the training. Not allowed by local department or fly in where is prohibited. Exceeding performance limits, such as ceiling, max speed, wind resistance, endurance, data link Not Safe limit. Extreme weather, such as thunderstorm, rain, typhoon, heavy fog. Flight planning does not comply with safety regulations. Taking off even not pass the pre-flight check. Exceeding the service life. CopyrightJOUAV 3 Contents Reading Tips..........................................................................................................................................1 Notation...........................................................................................................................................................1 Technical Support............................................................................................................................................1 Manuals List....................................................................................................................................................1 Safety Regulation...................................................................................................................................2 Warning...........................................................................................................................................................2 Attention..........................................................................................................................................................2 Disclaimer..............................................................................................................................................3 Summary................................................................................................................................................6 Features...........................................................................................................................................................6 Performance & Limitation...............................................................................................................................7 GCS-202..........................................................................................................................................................7 The Usage of CW-007 II System...........................................................................................................9 Assembly.........................................................................................................................................................9 Payload..........................................................................................................................................................15 Radio Controller............................................................................................................................................17 Battery...........................................................................................................................................................17 Lithium Ion Polymer Rechargeable Battery..................................................................................................17 The Function and Usage of GCS-202............................................................................................................24 CW Commander Ground Station Software...................................................................................................25 Accessories....................................................................................................................................................25 The Default Parameters.................................................................................................................................26 CW-007 II Operation Procedure..........................................................................................................27 Preparing.......................................................................................................................................................27 GCS-202 Installation.....................................................................................................................................27 Assembly and Check.....................................................................................................................................28 GCS Check and Mission Plan.......................................................................................................................28 Before Take Off.............................................................................................................................................30 After Take Off...............................................................................................................................................30 CopyrightJOUAV 4 Flying.............................................................................................................................................................31 Landing..........................................................................................................................................................32 After Landing................................................................................................................................................33 Data Download..............................................................................................................................................33 Maintenance and Update......................................................................................................................37 Fuselage Maintenance...................................................................................................................................37 Battery Maintenance......................................................................................................................................37 Aircraft and Accessories Update...................................................................................................................38 CopyrightJOUAV 5 Summary Features CW series UAV are kind of vertical take off and landing fixed wing UAV, which published by Chengdu JOUAV Automation Tech. Co., Ltd. And CW series UAV combined by fixed wing and quad-rotor, the maintenance is easy, and it has the property of long endurance, velocity, long range, and vertical take off and landing. The autopilot which is designed for CW Series UAV, and the UAV can take off, landing, and convert from fixed wing to multi-rotor or from multi-rotor to fixed wing automatically. Main Features Aerodynamic Configuration: Composited by quad rotor and fixed wing. High Efficiency: Assemble & Disassemble quickly, long endurance, velocity, long radius. VTOL: No need of runway. Easy to use: Auto take off and landing. Reliable: Complete alert & emergency logic RTK: Accuracy & Safety CopyrightJOUAV 6 Performance & Limitation CW-007 II Performance 2.2m 1.3m 19m/s 60min 800g
<3min 27m/s 16m/s Strong Breeze 4500m 6000m 6.8kg 30km 6 degrees Light rain (10mm/24h) Wingspan Length Cruise Speed Endurance Payload Time to expand/remove CW-007 II Limitation Max. Speed Stall Speed Wind Resistance Max. Take Off Height Ceiling MTOW Data Link Max. Climb Angle Rain-proof GCS-202 CopyrightJOUAV 7 GCS-20 02 commun nicated with h aircraft b by data link k, and commmunicated wwith GCS software byy Ch arging Port/
/ External B Battery Port t WiFi. Dat ta Link Ant tenna Wi Fi Antenna Pro oduct Mode el Har rdware Seri ial Number Pow wer Ch arge Status Pow wer Status RS 422 Port TX XD/ Data Tra ansmission RX XD/ Data Re eceiving Dat ta link signa al Wi Fi Status Chh arger Port/EExternal B aattery port, uused for chaarging or c oonnecting wwith a exter nnal battery. RSS 422 Port, uu se for downnloading B aase data, annd connecti nng with GCSS software bby cable, Funcctions an d updating the GCS-2002. TXX D status iss always lighht on. RXX D status iss about twi cce per seco nnd normally.. 8CopyrightJO OUAV The Usage oof CW-0007 II Sysstem Assembl ly Assembly p procedure a as below 1. Main w wing installa ation CopyrightJOUAV9 9 2. Multi-rotor installation 10CopyrightJOUAV 3. Left and right wings installation CopyrightJOUAV11 4. Elevator installation 5. Propellers installation 12CopyrightJOUAV 6. Battery installation CopyrightJOUAV13 7. Payload installation 14CopyrightJOUAV Payload d CA-100 camera is t the standard d payload f for CW-007 7 II, which is a full-fram me camera a develope ed for ae erial surveying. The main p parameters a are as follow ws:
CMOS S Size 35. 9 24. 0mm(F Full Frame)
) Resolu ution 7952 5304 Pixels Lens 42MP P 35mm m 1. Usage of Camera a On/Off f Po ower Memory card M Micro - SD c card Shutter Control Input HDMI Interface Sh hot Button Co Bo Po Si Co Bo onnect to th ox ower Supply ignal V=Cab onnect to th ox he Control y, Camera ble he Control Memory card On Offf Shutter Control Input All param meters have e been prese et at the fact tory. Sugge est to take sh hooting test t and confir m the effec t before ever ry flight. Be elow is the s setting:
ISO Apertu ure Shutter r Speed AU UTO (100-4 400) F 6 6. 3 1/1 1000 If th he photo is o overexpose d, increase the value of f shutter spe eed. It d doesnt matt ter if the ph hoto is not so bright but its clea ar, you can n adjust exp posure after r proc cessing. If t he IOS is to oo high, may ybe the pho oto will be o overexposure re. Copy rightJOUAV15 5 2. Camera Control Box and Settings When changing camera Settings and formatting memory CARDS, you need to use the camera control box to view and operate. The operation panel of the camera control box is shown below Usage of camera control box is:
1) Make sure the camera power is 2) Connect the HDMI cable and control 3) Turn on the camera power 4) Use the control box panel to set switched off cable parameters 5) Turn off the camera's power, and wait 30 seconds to re-start. Make sure the Settings are saved. 6) Turn off the power again and disconnect the cable Do not energize on or off the camera when the power switch is on!
3. Maintenance Storage: the CA-100 camera is recommended to be powered once a week. If it is not powered for a long time, please keep it dry and dust-proof. Transportation: please use packing box to transport and avoid inversion. 4. Other Payload For non - standard UAV, function and use of different payloads, please refer to the manual 16CopyrightJOUAV Radio C Controlle er We use th he TC-100 RC for CW W-007 II, ple ease refer to o the manual l of TC-100 0 RC. Battery 1. Batteri ies of CW-0 007 II Lithium Ion n Polymer R Rechargeab le Battery These w warnings and d safety tip ps are very important. Please rea ad them car refully. Wit thout strong g safety awar reness, imp proper opera ation may r result in pro oduct damag ge, property y loss, injur ry and even n 2. Safety t tip death. Th he battery should be used at a ambient tem mperature b between -1 10 and 5 50. High h temperatu ures (above e 60) may y cause batt teries to cat tch fire or e even explod de. If the tem mperature is s Copy rightJOUAV17 7 too low (less than 10), the performance of the battery will be reduced and cannot meet the requirements of normal use. Please start the heating function in advance, and it can be used normally when the temperature is restored. Battery charging environment temperature should be between 5 and 45, low temperature (below 5) charging will cause irreversible damage to the battery, even personal Please use the original charger for charge and discharge, do not charge and discharge when injury. unattended. If the battery falls from the UAV or is hit by external force, it shall not be used again. When removing batteries from the UAV, be sure to protect them from hitting the ground. Do not pull the handle strap violently. result in energy loss or failure to charge. If there is dirt in the battery socket, clean it with a dry cloth. Otherwise, poor contact can The liquid inside the battery is corrosive. If there is leakage, please stay away from it. If internal fluid spatters on human skin or eyes, rinse immediately with water and go to a doctor immediately. it may cause fire or explosion. the bottom of the battery. When the battery is not used properly, such as short circuit, overcharge, over discharge, etc. , When placing the battery, make sure the ground is flat to prevent sharp objects from poking The battery is heavy. Please place it carefully to prevent the battery from toppling and causing side damage. In case of battery damage, please immediately place the battery in an open area where is away from combustible materials and people. After half an hour, soak the battery in water for more than 24 hours. Ensure that the battery is completely exhausted before disposal. If the battery accidentally falls into the water during the flight of the UAV or under other circumstances, please pull out the battery immediately and place it in a safe and open area, and stay away from the battery until it is completely dried. Dry batteries are not allowed to be used again and should be disposed of properly in accordance with the waste method described in this 18CopyrightJOUAV article. In n case of b battery fire e, it is reco ommended to use fire e extinguish hing equipm ment in the e following g order: So oak it in w water with tools, sand d, fire blan nket, dry po owder, carb bon dioxide e extinguis sher. Do o not use ba atteries with h bulging, l eaking or d damaged pac ckaging. If the battery is in use or r charging
& discharg ging, remove e it from the e UAV or ch harger imm mediately and d discontinu ue use. Do o not use ba atteries in s trong static c or magnet ic fields. O Otherwise, th he battery c circuit board d may be ab bnormal, w which could lead to serio ous failure o of the UAV V. Do o not discha arge beyond d the maxim mum dischar rge current of the batte ery, or it ma ay cause fire e or explos sion. or other m metal object ts. Do o not use ba atteries near r a heat sour rce, such as in direct su unlight or in n a car on a hot day. It i is forbidden n to short-c ircuit the p ositive and negative el lectrodes of f the battery y with wires s It i is forbidden n to continu ue flying wh hen the batt tery power is less than n 15%, other rwise it wil ll cause bat ttery damag ge or cause f flight accide ent. Do o not disasse emble batte eries by you urself to avo oid danger. Do o not disass semble, pun ncture, impa act, collisio on, short cir rcuit the bat ttery or put t the battery y into fire, or it may ca ause fire or explosion. Do o not allow the battery to come int to contact w with any liqu uid. Do not immerse th he battery in n water or m make it wet t. Do not us se batteries in rain or h humid enviro onment. Co ontact with w water inside e the batter ry could lea ad to a dec composition n reaction th hat could c ause the ba attery to spo ontaneously y ignite or even explod de. Ba atteries are d dangerous s stuff. Do no ot pile other r things on the battery,
, or use the battery and d packagin g containin ng the batte ery as cush hion, otherw wise the b attery may y be damag ged or even n dangerou us. 3. Introdu uction and parameter rs Introdu uction Lithium Ion Polyme er Recharge eable Batter ry (hereinaf fter referred d to as smar rt battery) is s a specially y Copy rightJOUAV19 9 designed for the CW-007 II model with intelligent management system of smart battery. Smart battery has efficient low-temperature heating function and discharge storage function, and intelligent power management during flight. Compared with ordinary battery, energy utilization rate can be increased by 30%, thus improving operation efficiency. The smart battery uses a new high energy density battery cell and advanced battery management system to provide abundant power for the Adaptation of charger model: JIC-750A(CW-007 II standard charger), JICC-1500-A (Smart unmanned aircraft system. Parameters Model: JIB-18000A Rated capacity: 18000mAh Adaptation of UAV model: CW-007 II battery manager) Platform voltage: 22. 8V Battery type: lithium polymer battery 6S Energy: 410 Wh Weight: About 2. 2Kg Charging temperature: 5-45 Charging limit voltage: 26. 1V 4. Packing list Smart lithium battery X1 5. Description of appearance 20CopyrightJOUAV Function n button Status i ndicator lam mp Lo ock status in ndication Buckle e lock Charging b balance port Power c cord Nylon h handle Commu unication co onnector Sma art battery m manager bat ttery limit s slot The st tatus indicat tor is in ord der from left t to right: LE ED1LED D2LED3 LED4. 6. Battery y function Smart ba atteries have e the follow wing function ns:
Ba attery displa ay: Battery has its own n indicator light. Press once to ch heck the cur rrent battery y power and give an alar rm when the e capacity i s low. viewed thro ough the sof ftware of th he ground st tation. Int telligent com mmunicatio on: After co onnecting to o the aircra aft, the batte ery informa ation can be e Us sage record d: Managem ment system m can record d usage con nditions, su uch as max ximum load d, maximum a and minimu um usage tem mperature, discharge ti ime, etc. He eating funct tion: Help to o charge and d discharge e safely at lo ow temperat ture. Sto ore function n: Automati ic discharge e to storage capacity Copy rightJOUAV21 1 7. Operat tion guidan nce lock Sh hort press th he function n button
, the smart t battery sy ystem wake es up and d displays the e battery pow wer. When c charging, sh hort press th he function button once e
, the sta atus indicato or flashes to o indicate the e charging status. Whe en discharg ging, short p press the fu unction but tton once
, the status s indicator fl ashes to ind dicate disch harge status. While rest ing state, sh hort press th he function button once e
, witho out any oper ration, the s status indic ator will fla ash for 30s and the sys stem will au utomatically y shut down. Sh hort press th he function button wh hen display ying the pow werif the smart batte ery power is s lower than 20%, it wil l keep 30s a alarm remin nder (LED4 flashing re gularly). Wh hen the sma art battery s system wak kes up, and the state ind dicator is fl lashing, it c can enter the e heating mo de by pre essing the b button twice e continuous slywhich will prehea at the battery y. Wh hen the sm art battery system wak kes up, it ca an enter the e storage m mode by p pressing the e button 3 tim mes continu uously when n the status indicator fl flashesTh e smart bat ttery reache s the proper r storage cap pacity throug gh self-disc charge and a automaticall ly sleeps aft fter completi ion. Lo ong press th he function button it will termin nate all curr rent modes of smart ba attery, smar rt battery ente ers the sleep p state. station can view the ba attery inform mation. Af fter putting into the ai ircraft, the automatic e establishme ent of comm munication, the ground d 22CopyrightJ JOUAV 8. LED Status Indicator Status indicator can be used to display the battery charge and discharge process and other functional status, the indicator is defined as follows:
CopyrightJOUAV23 The Fun nction an nd Usag e of GCS S-202 1. Functio on of GCS-
-202 GCS-20 22 integrate dd with WiFii module, r aadio modulle and batt eery module. A nnd the acc eessories ar ee data link antenna, WWiFi anten nna, charger an dd the cabl ee for exter nnal battery. It can wor kk at most 66h with built-i n battery. Tripod i s used for installing the GCS-2202. If the GCS-202 is installed a tt a known point, makk e sure thee height off GCS-202 is measured bbefore flig hht. And thee height shhould be a s the pictuure shows. GCS S-202 Data a Link Anten nna WiFi iAntenna Tripo od WiFi Name WiFi Password IP Port 2. Charge e of GCS-20 02 Slant height is th e distance f from long si ide of upper r surface of f GCS-202 to o known po oint. After r power on the GCS-2 202, it will create a W Wi-Fi, which h is used fo for connecti ing between n CGS-20 02 and the l laptop. The setting abou ut network as blow:
G GCS202-190 09XXXX 1 909XXXX 1 0. 10. 100. 254 2 2010 There e is a charg ger for GC S-202, whi ch is conne ected AC p power and G GCS-202 fo or charging g. And the ere is a sign nal light of c charging sta atus. Conn nected betw een GCS-20 02 and char rger G Green R Red G Green Charg ging End o of charge 24CopyrightJ JOUAV A thr ree cells Li Po battery can provide e more wor rk time for GCS-202. If you need d to use the e external battery, make sure the built-in battery and the external one are full charged, and connect the external battery before power on the GCS-202. If the voltage is lower than 11. 2V, the GCS-202 will beep to remind you. Only three cells LiPo battery which can be used as external battery. CW Commander Ground Station Software There is a CW Commander software with CW Series UAV, which is used for checking aircraft, setting parameters, creating the flight plan, sending mission command, and so on. All the operations about CW Commander, please refer toCW Commander Manual. Accessories There are some software and cables for downloading data and update, such as autopilot recorder, autopilot update, GCS-202 update, PPS Process, RS-232 cable and RS-422 cable. The usage of these software refers to its manual. CopyrightJOUAV25 The Default Parameters Make sure all parameters have been checked before flight. And change some parameters if its necessary. For CW-20, the default parameters as blow(/means no need to change) :
Item Default Range Adjusting Condition 15-50 Increase if there is obstacle 1. 1-1. 2 High elevation Go around if lateral deviation is too much Landing Height 15-50 Increase if there is obstacle
>10
>10
Item Default Range Adjusting Condition Higher than ground about 50m Increase if there is obstacle Higher than Min. Altitude It all depends It all depends It all depends Timeout Limit 10min It all depends Flight Return 0 As total flight time Timeout Landing 2min
It all depends It all depends It all depends It all depends
*All items have been chosen except Line Safe Height, Min. Terrain Alt., Flight Return. Take off and Landing Set Minimum AGL Climb Coe. Lateral Deviation Height Deviation Clarify Acc. Cruise Speed Climb Speed 20 1. 1 10 10 1. 1 25 19 18 Deceleration Length 150 Emergency Parameters Min. Altitude Max. Altitude Line Safe Height Min. Terrain Alt. 660 6000 0 70 26CopyrightJOUAV CW-007 II Operation Procedure We suggest that the aircrew consists of 1 or 2 people, and the aircrew operate this UAV system as blow procedures. One of them who in charge of the ground control station, the rest people who check the aircraft and prepare for the emergency situation. And only one person can also finish all the operation. Preparing Battery:Make sure all the batteries are full charged, including aircraft, radiocontroller, GCS-202, laptop, external battery for GCS-202. CWCommander:Load the map of mission area. Create the flight plan and check the elevation before flight to save time when youre outside. Aircraft:Confirm no damageduring storage or transportation, and allcomponents are correctly positioned in the backpack case. Do not put desiccant and other little things into the flight case when transport the case. GCS-202 Installation Confirm the WiFi antenna and the data link antenna are fixed, and then install the GCS-202 to the tripod. If its needed, connect the external battery to increase work time. And then, power on the GCS-202. Measure the slant height or connect the fiber glass antenna if its needed. The GCS-202 should be far from ground, vehicles, buildings. CopyrightJOUAV27 Assembly and Check 1. Assembly 2. Check Aircraft Open the flight case, assemble the aircraft as the procedures All cabin lids and hinges are no damages. Pitot:The pitot is fixed. No break, no blockage. Fuselage:The body and wings are no damages. The screw holes of wings and tails are no damages. Assembly:Rotors arm are fixed and correct, cabin lids are fixed, wings are fixed. Control Surfaces:All the control surfaces are no damages, all the servos are fixed, the connecting between servos and control surfaces are fixed. Rotors Power:The rotors are fixed, propellers are no damages and fixed. Forward Power: Propeller no damage, and the cover is locked tightly. Avionics:All the connectors and cables of autopilot, engine, and rotors are no damages. Payload is fixed. 3. Battery Installation Antennas of Aircraft:The data link antenna and others are fixed. Install the batteries and payload after checking the aircraft. Then, power on the autopilot. GCS Check and Mission Plan Make sure the Radio Controller in ATT. Mode before power on the autopilot. If you dont have any experience about RC, you can switch off the RC. And skip all the steps about the RC. 1. Check Parameters and Status Common Status:Telemetry is good, RC status is correct, sensor self-check passed, aircrafts position is correct, instrument attitude is correct. Batteries:The main power and GCS power are enough for flight, the servo power is about 6V. Airspeed:Airspeed should be 0 or almost same with the wind speed. 28CopyrightJOUAV Take Off and Landing Set: Minimum AGL and Landing Height are depending on flight site. If the ground elevation is higher than 2000m, increase the Climb Coe., and normally we dont have to change other parameters. you need. 2. Compass Calibration Emergency Parameters:Make sure the Min. Altitude is correct, and change other parameters if Task Setting:Confirm the Spacing or Timing, and make sure the Hold Time is correct. We suggest calibrating the compass before every flight if the flight site is changed. If you fly at the same place as last time, you dont have to calibrate but must check the compass in Pre-flight Check. After calibration, save data to autopilot. If the Error is more than 10 degrees(which is in Objects), restart the autopilot and check again. When calibrating and inspecting the compass, keep the aircraft away from vehicles, iron towers, on the metal table or concrete floor with steel bars. 3. Create Flight Plan If the flight plan has been created before mission, you can import the plan, and make sure the spacing or timing is correct. Aftercreating flight plan, must adjust the waypoint 0, waypoint 1, the last but one(Penultimate)waypoint and the last waypoint. Check the height of flight plan, make sure the flight plan is higher than ground at least 100m, the last waypoint is higher than ground 100-150m. Send the plan to autopilot after finish checking, and then request the flight plan to confirm its correct. 4. Create Landing Plan Make sure the landing direction is heading the wind and no obstacle. The landing plan area should be empty and far from the buildings, big trees, power towers and mountains. The landing position should be clear and far from aircrew and tripod. And the aircraft will not fly over the people when its taking off or landing. After finishing the creating landing plan, must check the height of landing plan to make sure its safe. CopyrightJOUAV29 Pre-fligh ht Check:D Do the chec cklist one by y one. Do n not take off ff if any che eck items fa failed on the e Before T Take Off:R Remove the pitot cover r, confirm th he aircraft i is heading t the waypoin nt 1 and the e wind direct tion. Make sure the su urrounding i is clear, swi itch the RC C to AUTO mode. Then n send Take e Before T Take Off f checklist. Off comma and. After Ta ake Off After the e aircraft lift ft off, the op peratorneeds s to monitor r the flight d data and sta atus, as follo ows:
Power:T The power s system may not provide e enough po ower for mu ulti-rotor be ecause the te emperature is too low, e elevation is too high, b battery aging g. And if tha at happens, the aircraft t will land automatical lly. Either y you can send d Abort to o make it la and right no w. Airspeed d:The airsp eed should be same wi ith the wind d speed and stable when n its climbi ing out. If the airspeed d is increasi ing and mor re than 10m m/s, that may y was cause ed by pitot f failure, and send Abort to land right n now. force landin ng. current position. Abort to make it forc ce landing. Accelera ating: In th e process o f acceleratio on, if any a abnormal co onditions. S end Abort to make i t Force e landing, w which means s the aircra aft transform m from fixed d wing to m multi-rotor, and land a t Others In multi-ro otor workin ng condition n, other rea asons for th e need to a abort the mi ission. Send d 30CopyrightJ JOUAV Flying After aircraft goes to mission plan, please switch off the RC. And the operator of GCS should keep monitoring the flight status, especially the altitude, vertical speed, airspeed, ground speed, voltage, attitude, telemetry etc. Altitude:The altitude should keep increasing during climbing up. If the aircraft lose height more than 20m, it will go back to waypoint 0. If the aircraft lose height and lower than Min. Altitude or lose height more than Safe Line Height, it will force landing. (If Safe Line Height has been chosen. ) Vertical Speed:The vertical speed should be a positive value during climbing up, and is the range of 2-4m/s usually. If its negative value during climbing up, land the aircraft as soon as possible. The vertical speed should be near 0 during climbing up Airspeed:The cruise speed is 19m/s, and the climb speed is 18m/s. The telemetry speed should be almost same with target speed. The target airspeed is calculated by autopilot which based on the sea level and standard atmospheric pressure(Indicating airspeed/IAS). The autopilot can calculate the altitude and automatically modify the airspeed. So the target airspeed should be higher with the altitude increasing (true airspeed/ TAS). The telemetry speed should be almost same with target speed Ground Speed:The ground speed should change with wind speed. If the difference between ground speed and wind speed is more than 10m/s, that means the wind is too strong, and we suggest to cancel the mission and land. Voltage: The full voltage of main power is 25. 2V, land if its lower than 21. 6V. The voltage of servo power is 5. 5-6. 0V normally. If the main power is lower than return voltage more than 10s, the aircraft will go back to waypoint 0 automatically Attitude:The maximum roll angle should be less than 35 degrees, the maximum pitch angle should be leess than 15 degrees. If it is not, thee software wwill show yyou red coloor on attitudee to remindd. CopyrightJOUAV31 Data Link:If th he data lin nk is disco nnected, th he RX wil ll stop incr reasing wh hich on the e CWComma ander. If the e time after r disconnect ted data lin nk is more th han time ou ut limit sett ting, aircraf ft will return to waypoin nt 0. If the a aircraft is f far from the e take off po oint more th han 1km an nd the fligh ht time is mor re than time eout return setting, it w will return to o waypoint 0. If the da ata link is d disconnected d more than t timeout land ding setting g and its far r from the la anding poin nt less than 2 2km, it will l trace to the e landing pla an and land a automatical lly. Landing g Before la anding, the operator sh ould confirm m the status s, such as la anding comm mand, APm mode, altitude, tar rget waypoi nt, rotors po ower. The pilot t should con nfirm the R RC is auto m mode, and k keep the thro ottle minim mum, then sw witch on the e RC, push th he throttle t o middle. A And confirm m the contro l status is R RC Normal and throttle e is about 50 0%
with operat tor of GCS. 797, and th hen rotate th he landing p plan. If the wind direct tions has ch hanged, pre ess shift and d left button n of mouse t to choose th he waypoin t After sen nding Land ding comm mand, the op perator shou uld pay atten ntion to alti tude, rotors s power and d APmode. In n addition, d data and co nditions nee ed to pay at ttention, as follows:
Fixed W Wing Status
:If the altitu ude of aircra aft is lower r than Landi ing Height, it will force e landing. I f the aircraft is always g going around d, increase t the Lateral Deviation. Multi-ro otor Status
:While the aircraft is h hovering bu ut not desce ending, it w will land afte er 20s if the e distance be etween aircr raft and land ding point i s no more t than 10m. a and it will fo orce landing g after 1min n if the distance is more than 10m. Either you can send Landing command to land it. Touch Ground:After touching ground, keep the throttle minimum, and switch the RC to ATT mode. If the propeller keeps running and not stop, send Abort to stop it. 32CopyrightJ JOUAV After Landing After landing, disconnect the rotors power and engine power, switch off the RC. And then download the POS data if its needed. Must download POS data before power off the autopilot, or the next flight will cover the last POS data. If the autopilot is off, you can input photo number manually. And we suggest downloading the rover data and base data after every flight. Data Download 1.Download POS data from Airborne Step 1: when the UAV is power off, use the data download cable to connect the computer and the UAV. The data download cable is adjusted to Norm-422 Step 2: open the Recorder software, select the serial number and set the baud rate by default. Step 3: power on the UAV, and after 5 seconds, switch Norm to Boot. CopyrightJOUAV33 Step 4
: click "con nnect", the d download u unit appears s after the c connection is establish hed, find the e downlo oad unit cor rresponding g to the flig ght period, a and enter th he number of the unit into "unitto o downlo oad" below. Step 5:
: click the "s start" button n and wait f for the down nload to com mplete. Step 6 6: after the download is complet ted, enter t the next re quired dow wnload unit t number to o downlo oad. After d downloading g all the dat ta, click "Lo ogout" to dis sconnect th e data down nload cable
. Step 7:
: power off the UAV, fi inish the dow wnload Th he download ded file is n named rove er beginnin ng file, whi ich is stored d in the outp put folder in n the e directory o of Recorder r software. Note:
2.Downloadd POS data from GCS--202 1. Afte r download ding, the rec corder shoul ld be restart ted before it t can be use ed again. 34CopyrightJ JOUAV Step 1: w when the gro ound station n is shut do own, connec ct the comp puter and gr round base station with h the data d download ca able, and ad djust the dat ta download d cable to N Norm-422 Step 2:
: open the R Recorder sof ftware, sele ct the serial l number an nd set the ba aud rate by d default Step 3:
: start up the e ground sta ation and cl ick "connec ct". click "c connect", th he download d unit appea ars after the e connection n is establis hed, find th he download d unit co orresponding g to the flig ght period, a and enter th he number o of the unit i into "unit to o download"
Step 5:
: click the "s start" button n and wait f for the down nload to com mplete. Step 6 6: after the download is complet ted, enter t the next re quired dow wnload unit t number to o downlo oad. After a all data is do ownloaded, the softwar re can be clo osed directly y. Step 7 7: shutdown n the grou nd station, disconnec t the data download cable, and d finish the e below. downlo oad. Th he download ded file is n named bas e beginnin ng file, whic ch is stored d in the outp put folder in n the e directory o of Recorder r software. Copy rightJOUAV35 5 Note:
1. After downloading, the recorder should be restarted before it can be used again. 2. After downloading the data, power off the autopilot, and then clean the aircraft, disassemble the aircraft and put into backpack case correctly. 36CopyrightJOUAV M Mainten nance and d Updat te Sugge est take fligh ht practice a at least once e a month to o maintain o operational proficiency y. Fuselage e Mainte enance Clean t the fuselage e after every y flight. Cov ver the pitot t when stori ing the aircr raft. Keep th he case is d dry when sto oring. Battery Mainten nance The sto orage wet is s 6520%, s storage temp perature is -
-20-35
. Storage e time no m more than 7 d days if the v voltage is h igher than 3 3. 9V/Cell. Every 3 3 months cy ycle the batt tery while s storing. Norma ally, the disc charge capa city will dim minish after r 100 cycles s. If the d discharge ca apacity dim minishes too o much, disc charge the b battery, and d soak it in salty water r, Use in low temper rature or hig gh elevation n place, mak ke sure war rm the batte ery up befor re taking of ff then se end it to recy ycle bin. and kee ep it warm during flyin ng. Copy rightJOUAV37 7 Aircraft and Accessories Update The customer will receive the update file from JOUAV if it is need to be updated. We suggest updating the autopilot immediately if customer receive the update. If there is new version of CWCommander, the software will remind you when you start it. And if you choose update, it will download and install automatically. We will send the update to customer if its needed to be updated. And we suggest updating 1. Autopilot 2. CWCommander 3. GCS-202 immediately. 4. Others new version. The POS processing software, update software and so on. We will send to customer if there is For CW-007/GCS-202 (Unmanned Aerial Photography UAV) FCC Statement:
Any Changes or modifications not expressly approved by the party responsible for compliance could void the users authority to operate the equipment. This device complies with part 15 of the FCC Rules. Operation is subject to the following two conditions:
(1) This device may not cause harmful interference, and
(2) This device must accept any interference received, including interference that may cause undesired operation. FCC Radiation Exposure Statement:
This equipment complies with FCC radiation exposure limits set forth for an uncontrolled environment. This equipment should be installed and operated with minimum distance 20cm between the radiator& your body. Note: This equipment has been tested and found to comply with the limits for a Class B digital device, pursuant to part 15 of the FCC Rules. These limits are designed to provide reasonable protection against harmful interference in a residential installation. This equipment generates, uses and can radiate radio frequency energy and, if not installed and used in accordance with the instructions, may cause harmful interference to radio communications. However, there is no guarantee that interference will not occur in a particular installation. If this equipment does cause harmful interference to radio or television reception, which can be determined by turning the equipment off and on, the user is encouraged to try to correct the interference by one or more of the following measures:
Reorient or relocate the receiving antenna. Increase the separation between the equipment and receiver. Connect the equipment into an outlet on a circuit different from that to which the receiver is connected. Consult the dealer or an experienced radio/TV technician for help. 38CopyrightJOUAV
1 2 | FCC ID Label | ID Label/Location Info | 630.22 KiB | August 11 2020 |
ProductName:Ground Control Station Model: GCS-202 Input: DC 12.6V SN:XXXXXX FCC ID: 2AVXCGCS-202 CHENGDU JOUAV DA PENG TECH CO., LTD Add: 6A-7F, Jingrong Innovation Hub, No. 200 5th TianFu St., Hi-tech District, Chengdu, 610000 China Made in China
1 2 | Confidentiality Letter | Cover Letter(s) | 86.49 KiB | August 11 2020 |
Company: CHENGDU JOUAV DA PENG TECH CO., LTD Add: 6A-7F, Jingrong Innovation Hub, No. 200 5th TianFu St., Hi-tech District, Chengdu, 610000 China Tel: 028-84191660 Fax: 028-62711135 E-mail: Penghaiyan@jouav.com FCC Confidential Authorization Date:2020-03-10 FEDERAL COMMUNICATIONS COMMISSIONS Authorization and Evaluation Division 7435 Oakland Mills Road Columbia, MD 21046 Subject: Confidentiality Request regarding application for certification of FCC ID: 2AVXCGCS-202 To: whom it may concern, In accordance with Sections 0.457 and 0.459 of the Commissions Rules, CHENGDU JOUAV DA PENG TECH CO., LTD hereby requests long-term confidential treatment of information accompanying this application as outlined below:
The above materials contain proprietary and confidential information not customarily released to the public. The public disclosure of these materials provides unjustified benefits to its competitors in the market. Block Diagram Schematics Operation Description Sincerely Yours, Signature:
Typed or Printed Name: Haiyan Peng Title: overseas sales director
1 2 | Power of Attorney Letter | Cover Letter(s) | 64.61 KiB | August 11 2020 |
Company: CHENGDU JOUAV DA PENG TECH CO., LTD Add: 6A-7F, Jingrong Innovation Hub, No. 200 5th TianFu St., Hi-tech District, Chengdu, 610000 China Tel: 028-84191660 Fax: 028-62711135 FCC Authorization Date: 2020-03-10 FEDERAL COMMUNICATIONS COMMISSION Authorization and Evaluation Division 7435 Oakland Mills Road Columbia, MD 21046 Subject: Agent Authorization To whom it may concern:
We, CHENGDU JOUAV DA PENG TECH CO., LTD, the undersigned, Hereby authorizes Bay Area Compliance Laboratories Corporation to act on its behalf in all matters relating to application for Equipment authorization, including the signing of all documents relating to these matters. All acts carried out by Bay Area Compliance Laboratories Corp. on our behalf shall have the same effect as our own action. We, the undersigned, hereby certify that we are not subject to a denial of federal benefits, that includes FCC benefits, pursuant to Section 5301 of the Anti-Drug Abuse Act of 1988, 21 U.S.C. 862. This authorization is valid until further written notice from the applicant. Sincerely Yours, Signature:
Typed or Printed Name: Haiyan Peng Title: overseas sales director QA-FR-170-B
frequency | equipment class | purpose | ||
---|---|---|---|---|
1 | 2020-08-11 | 2401.6 ~ 2477.6 | DSS - Part 15 Spread Spectrum Transmitter | Original Equipment |
2 | 2412 ~ 2462 | DTS - Digital Transmission System |
app s | Applicant Information | |||||
---|---|---|---|---|---|---|
1 2 | Effective |
2020-08-11
|
||||
1 2 | Applicant's complete, legal business name |
CHENGDU JOUAV DA PENG TECH CO., LTD
|
||||
1 2 | FCC Registration Number (FRN) |
0029318912
|
||||
1 2 | Physical Address |
6A-7F, Jingrong Innovation Hub, No. 200 5th TianFu St., Hi-tech District
|
||||
1 2 |
6A-7F, Jingrong Innovation Hub, No. 200
|
|||||
1 2 |
Chengdu, N/A
|
|||||
1 2 |
China
|
|||||
app s | TCB Information | |||||
1 2 | TCB Application Email Address |
b******@baclcorp.com
|
||||
1 2 | TCB Scope |
A4: UNII devices & low power transmitters using spread spectrum techniques
|
||||
app s | FCC ID | |||||
1 2 | Grantee Code |
2AVXC
|
||||
1 2 | Equipment Product Code |
GCS-202
|
||||
app s | Person at the applicant's address to receive grant or for contact | |||||
1 2 | Name |
H**** P******
|
||||
1 2 | Title |
overseas sales director
|
||||
1 2 | Telephone Number |
028-8********
|
||||
1 2 | Fax Number |
028-6********
|
||||
1 2 |
P******@jouav.com
|
|||||
app s | Technical Contact | |||||
n/a | ||||||
app s | Non Technical Contact | |||||
n/a | ||||||
app s | Confidentiality (long or short term) | |||||
1 2 | Does this application include a request for confidentiality for any portion(s) of the data contained in this application pursuant to 47 CFR § 0.459 of the Commission Rules?: | Yes | ||||
1 2 | Long-Term Confidentiality Does this application include a request for confidentiality for any portion(s) of the data contained in this application pursuant to 47 CFR § 0.459 of the Commission Rules?: | No | ||||
if no date is supplied, the release date will be set to 45 calendar days past the date of grant. | ||||||
app s | Cognitive Radio & Software Defined Radio, Class, etc | |||||
1 2 | Is this application for software defined/cognitive radio authorization? | No | ||||
1 2 | Equipment Class | DSS - Part 15 Spread Spectrum Transmitter | ||||
1 2 | DTS - Digital Transmission System | |||||
1 2 | Description of product as it is marketed: (NOTE: This text will appear below the equipment class on the grant) | Ground Control Station | ||||
1 2 | Related OET KnowledgeDataBase Inquiry: Is there a KDB inquiry associated with this application? | No | ||||
1 2 | Modular Equipment Type | Does not apply | ||||
1 2 | Purpose / Application is for | Original Equipment | ||||
1 2 | Composite Equipment: Is the equipment in this application a composite device subject to an additional equipment authorization? | Yes | ||||
1 2 | Related Equipment: Is the equipment in this application part of a system that operates with, or is marketed with, another device that requires an equipment authorization? | Yes | ||||
1 2 | Grant Comments | Output power listed is conducted. The antenna(s) used for this transmitter must be installed to provide a separation distance of at least 20 cm from all persons and must not be co-located or operating in conjunction with any other antenna or transmitter. Users and installers must be provided with antenna installation instructions and transmitter operating conditions for satisfying RF exposure compliance. This device supports 20 MHz and 40 MHz bandwidth modes. | ||||
1 2 | Is there an equipment authorization waiver associated with this application? | No | ||||
1 2 | If there is an equipment authorization waiver associated with this application, has the associated waiver been approved and all information uploaded? | No | ||||
app s | Test Firm Name and Contact Information | |||||
1 2 | Firm Name |
Bay Area Compliance Laboratories Corp. (Chengdu)
|
||||
1 2 | Name |
M**** C********
|
||||
1 2 | Telephone Number |
+86 0********
|
||||
1 2 |
q******@baclcorp.com
|
|||||
Equipment Specifications | |||||||||||||||||||||||||||||||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Line | Rule Parts | Grant Notes | Lower Frequency | Upper Frequency | Power Output | Tolerance | Emission Designator | Microprocessor Number | |||||||||||||||||||||||||||||||||
1 | 1 | 15C | 2401.60000000 | 2477.60000000 | 0.0460000 | ||||||||||||||||||||||||||||||||||||
Line | Rule Parts | Grant Notes | Lower Frequency | Upper Frequency | Power Output | Tolerance | Emission Designator | Microprocessor Number | |||||||||||||||||||||||||||||||||
2 | 1 | 15C | 2412.00000000 | 2462.00000000 | 0.0530000 |
some individual PII (Personally Identifiable Information) available on the public forms may be redacted, original source may include additional details
This product uses the FCC Data API but is not endorsed or certified by the FCC