Idea-fly Hero-550 Manual de usuario

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Hero-550
C6W—FlightControlSystem
UserManualv1.0

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Disclaimer
Pleasereadthisdisclaimercarefullyandfollowinstructionsonassemblyandcalibrationcontained
inthismanual.Byusingourproduct,youherebyagreetothisdisclaimerandsignifythatyouhave
readtheentiremanualthoroughly.
THISPRODUCTISNOTSUITABLEFORPEOPLEUNDERTHEAGEOF18.
Thisproductisnotatoy!Itisacomplicatedcombinationofmechanics,electronics,aerodynamics
and high-frequency radio technologies. Users should strictly obey safety operation specification on
aerialmodelandfollowstepsillustratedinthemanualtoinstallandcalibratetheproduct.Idea-Fly
takesnoresponsibilityforanydirectorindirectdamage(s)orinjuriescausedbyimproperinstallation,
calibrationandoperation.
Idea-Fly takes no responsibility for any direct or indirect damage(s) or injuries caused by
installing/calibrating/flying this product when users are in situations including butnot limited like
drunk,takingdrugs,dizziness,fatigueoranyothercasesnomattermentallyorphysicallythatwould
impairyourability.
Idea-Flytakesnoresponsibilityforanydirectorindirectdamage(s)orinjuriescausedbyflyingthis
productininappropriatewhetherlikewindy(nomorethangentlewind),rain,snow,hail,lightningor
anynaturaldisaster.
Idea-Flytakesnoresponsibilityforanydirectorindirectdamage(s)orinjuriescausedbyusingthis
productininappropriatearealikemagneticorradiointerferencearea,governmentregulatedno-fly
zoneoranyothernotpermittedpublicorprivateareas.
Idea-Flytakesnoresponsibilityforanydirectorindirectdamage(s)orinjuriescausedbyusingthis
productassembledwithpartsNOTproducedbyIdeaFly,incomplete/incorrectassemblyorIdea-Fly

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productinagingorerodedcondition.
Ifanyquestionsorproblemsoccurbefore,duringorafterusingIdea-Flyproducts,pleasecontact
local distributor/seller or Idea-Fly customer service for answers or assistance. Idea-Fly takes no
responsibility for any direct or indirect damage(s) or injuries caused by customer’s improper
operationorsubjectivemisjudgment.
AnyotherlossesthatarenotIdea-Fly’sliability.
Flightcontroller
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HardwareInstallationandConnection
1)HardwareConnectionDiagram:
2)PortDescription:

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Interface DefinitionofEachPin Interfacefunction
AIL Signal
5V GND ToAILofRCRx
ELE signal
5V GND ToELEofRCRx
THR signal
5V GND ToTHRofRCRx
RUD signal
5V GND ToRUDofRCRx
CH5 signal
5V GND ToCH5ofRCRx
CH6 signal
5V GND ToCH6ofRCRx
POW 1.5V 5V GND Connectto5V/2ADCmodule
LED B G R LEDModule
USB ConnecttoPC
M1 signal ESCoutput GND ToESCofMotor1
M2 signal ESCoutput GND ToESCofMotor2
M3 signal ESCoutput GND ToESCofMotor3
M4 signal ESCoutput GND ToESCofMotor4
M5 signal ESCoutput GND ToESCofMotor5
M6 signal ESCoutput GND ToESCofMotor6
Y1 signal 5V GND TogimbalRollServo
Y2 signal 5V GND Togimbalpitchservo
GPSR TXD 3.3V RXD ToGPSport1(Redterminal)
GPSB SDA GND SCL TOGPSport2(Blackterminal)

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3)PortConnection
WHITEcorewireisalwaysthesignalline,theREDcorewireispositive;theBLACKcorewireis
ground
4)Notice:
①SupportQuad-Rotor1andQuad-RotorX
As shown,M1-M4 correspond to the output ports(M1~M4) on the Main Controller(MC). The

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directionofthearrowindiagramindicatestherotationdirectionofthemotor/propeller.
② forMaincontroller:
M1-M4portshouldpointtothenoseofaircraft
Maincontrollersidesshouldbeparalleltotheaircraftbody.
③ ForGPS&COMPASSModule:
Thearrowshouldpointtothenosedirectionofaircraft
GPS /compass is sensitive to magnetic interfence, should be far away from any electronic
devices.Ifyourownmountingrod.makesureitisNOTmagnetic.
When you find the aircraft rotating or drifting, Please check the GPS module mounting
orientationandthenre-dothecompasscalibration.
Installingandrunningonwindow
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1.“Read” Button
Download the current parameters, Usually, the default parameters are good enough for the
flights.
2.“save “ Button
① Turnonthetransmitter,Switch3positionswitchtoRTHmode.
Thenpoweronyouraircraft.after3secs.ConnectyouraircraftandPCviaMicro-USBcable.
Notice:Forfirmwareupdate:connecttheUSBcablefirstandthenpoweronyouraircraft.
②Runtheassistantsoftware”IDEAFLY-GCS.ex”(asshown)
③thenclick”openUSB”

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Edittheparameters: Click “save” Button” tosavethenewestparameters.(Ifthisfailstry
severaltimes)
3. ” Default” Button
Different multi-rotors have different gains because of different motor KV ratings, ESC and
propellersize.Sodefaultparametersisn’tforHero-550.
4.Hero-550parametersareshownbelow.
① Roll/Pitch sensitivity is used to adjust the compensation angle of the PTZ data for your
Gimbal.
(Note: range -127 to 127,You can enter a negative value to reverse the direction of
compensation).
② Roll-Stab and Pitch-stab would affect the degree of command response in flight (range
0-255),
Shake-Compenscanincreasestabilitybutwoulddecreasethesensitivity(range0-255).
③ Altitude/DistanceLimit:Themaximumheightanddistanceallowedcanbespecified.min10
meters.
④ Enter this to match the frequency ofyour gimbal servos. 50Hz, 250Hz, 333Hzand 400Hz
servosaresupported.

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⑤ numberofcells
⑥ Inordertopreventyourmulti-rotorfromacrashorotherharmfulconsequencescausedby
lowbatteryvoltage ,therearetwolevelsoflowbatteryprotectionavailabletouse.
MakesureCarefullyreadLipoBatterySafetyGuide:
*********************************************************
Notice:LIPOBatteriesandLIPOchargersCANigniteandcausefire.
ThesecautionsMUSTbefollowed
1.NeverchargeaLIPObatteryifitishottothetouch.
2.NeverchargeadamagedorbrokenLIPOBattery.
3.ONLYCHARGEONAFIREPROOFSURFACE.
4.DONOTCHARGEUNATTENDED.
Enterthevoltagepercellrequiredtoactivatealowvoltagealert,foraLipobatterythiswould
benormallybe3.65v.
Note:
1、BothlevelsofprotectionhaveLEDwarningasdefault.Bothlevelsofprotection
willblinkredcontinuously.
2、Whenthereisnopower,aircraftwillauto-land.
3、TheMCcancalculatefinalstagelowvoltageaccordingtotheCellNumberandFirststage
lowvoltagealert Finalstagevalue=(Firststagelowvoltagealert-0.05v)*CellNumber

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5.Donotuseorchargeifwet.
6.Donotuseorchargeifthebatteryhasexpanded,enlarged,orswelled.
7.Neverdischargebelow3.0Vpercell.
8.Neverchargeabatterythathasbeendischargedbelow3.0Vpercell.
⑦SetuptheMaximumrateofclimbanddescent.
⑧ Setupthemaximumflightspeed.
⑨ Mode : Include manual, manual set altitude, GPS set altitude, GPS set altitude
(head-free),Returnandland.
FlightModeDescription
1 、Manual
InManualMode,theaircraftwillflynormallyandisstabilizedin3axes.
TheaircraftmaybecontrolledbyTX,butisalsocontrolledbythestabilizationsignalofmain
controller. The final flying state is determined by a combination of manual control and MC
control.
2 、Manualsetaltitude
Inthismode,craftwillholdthealtitudebutnotholdtheposition.
WhentheTHRstickisinits50%positionthecraftwillhoverinthecurrentaltitudebut
notatitscurrentposition(thecraftwilldriftwhentheGPSisnotlocked),butthecraft
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