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https://github.com/ArduPilot/ardupilot
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Airspeed: store reference in libraries and populate it
- also had to move the initial definition in plane.h so it happened before the others.
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@ -159,6 +159,9 @@ private:
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// mapping between input channels
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RCMapper rcmap;
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// Airspeed Sensors
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AP_Airspeed airspeed;
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// board specific config
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AP_BoardConfig BoardConfig;
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@ -221,12 +224,12 @@ private:
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#endif
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AP_L1_Control L1_controller {ahrs};
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AP_TECS TECS_controller {ahrs, aparm};
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AP_TECS TECS_controller {airspeed, ahrs, aparm};
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// Attitude to servo controllers
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AP_RollController rollController {ahrs, aparm, DataFlash};
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AP_PitchController pitchController {ahrs, aparm, DataFlash};
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AP_YawController yawController {ahrs, aparm};
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AP_RollController rollController {airspeed, ahrs, aparm, DataFlash};
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AP_PitchController pitchController {airspeed, ahrs, aparm, DataFlash};
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AP_YawController yawController {airspeed, ahrs, aparm};
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AP_SteerController steerController {ahrs};
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#if CONFIG_HAL_BOARD == HAL_BOARD_SITL
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@ -393,9 +396,6 @@ private:
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AP_Frsky_Telem frsky_telemetry {ahrs, battery};
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#endif
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// Airspeed Sensors
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AP_Airspeed airspeed;
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// ACRO controller state
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struct {
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bool locked_roll;
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@ -10,7 +10,8 @@
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class AP_PitchController {
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public:
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AP_PitchController(AP_AHRS &ahrs, const AP_Vehicle::FixedWing &parms, DataFlash_Class &_dataflash) :
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AP_PitchController(AP_Airspeed &aspeed, AP_AHRS &ahrs, const AP_Vehicle::FixedWing &parms, DataFlash_Class &_dataflash) :
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airspeed(aspeed),
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aparm(parms),
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autotune(gains, AP_AutoTune::AUTOTUNE_PITCH, parms, _dataflash),
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_ahrs(ahrs)
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@ -37,7 +38,7 @@ public:
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private:
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const AP_Vehicle::FixedWing &aparm;
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AP_Airspeed airspeed;
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const AP_Airspeed &airspeed;
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AP_AutoTune::ATGains gains;
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AP_AutoTune autotune;
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AP_Int16 _max_rate_neg;
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@ -10,7 +10,8 @@
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class AP_RollController {
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public:
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AP_RollController(AP_AHRS &ahrs, const AP_Vehicle::FixedWing &parms, DataFlash_Class &_dataflash) :
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AP_RollController(AP_Airspeed &aspeed, AP_AHRS &ahrs, const AP_Vehicle::FixedWing &parms, DataFlash_Class &_dataflash) :
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airspeed(aspeed),
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aparm(parms),
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autotune(gains, AP_AutoTune::AUTOTUNE_ROLL, parms, _dataflash),
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_ahrs(ahrs)
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@ -44,7 +45,7 @@ public:
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private:
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const AP_Vehicle::FixedWing &aparm;
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AP_Airspeed airspeed;
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const AP_Airspeed &airspeed;
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AP_AutoTune::ATGains gains;
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AP_AutoTune autotune;
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uint32_t _last_t;
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@ -9,7 +9,8 @@
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class AP_YawController {
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public:
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AP_YawController(AP_AHRS &ahrs, const AP_Vehicle::FixedWing &parms) :
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AP_YawController(AP_Airspeed &aspeed, AP_AHRS &ahrs, const AP_Vehicle::FixedWing &parms) :
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airspeed(aspeed),
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aparm(parms),
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_ahrs(ahrs)
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{
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@ -29,7 +30,7 @@ public:
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private:
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const AP_Vehicle::FixedWing &aparm;
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AP_Airspeed airspeed;
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const AP_Airspeed &airspeed;
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AP_Float _K_A;
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AP_Float _K_I;
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AP_Float _K_D;
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@ -29,7 +29,8 @@
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class AP_TECS : public AP_SpdHgtControl {
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public:
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AP_TECS(AP_AHRS &ahrs, const AP_Vehicle::FixedWing &parms) :
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AP_TECS(AP_Airspeed &aspeed, AP_AHRS &ahrs, const AP_Vehicle::FixedWing &parms) :
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airspeed(aspeed),
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_ahrs(ahrs),
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aparm(parms)
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{
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@ -121,7 +122,7 @@ private:
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AP_AHRS &_ahrs;
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const AP_Vehicle::FixedWing &aparm;
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AP_Airspeed airspeed;
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const AP_Airspeed &airspeed;
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// TECS tuning parameters
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AP_Float _hgtCompFiltOmega;
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