AC_AttControl: remove example sketch
This sketch only tested compiling anyway
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/*
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* Example of AC_AttitudeControl library
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* DIYDrones.com
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*/
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#include <AP_Common.h>
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#include <AP_Progmem.h>
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#include <AP_Math.h> // ArduPilot Mega Vector/Matrix math Library
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#include <AP_Curve.h> // Curve used to linearlise throttle pwm to thrust
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#include <AP_Param.h>
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#include <AP_HAL.h>
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#include <AP_HAL_AVR.h>
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#include <AP_GPS.h> // ArduPilot GPS library
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#include <AP_GPS_Glitch.h> // GPS glitch protection library
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#include <AP_ADC.h> // ArduPilot Mega Analog to Digital Converter Library
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#include <AP_ADC_AnalogSource.h>
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#include <AP_Baro.h> // ArduPilot Mega Barometer Library
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#include <AP_Baro_Glitch.h> // Baro glitch protection library
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#include <Filter.h>
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#include <AP_Compass.h> // ArduPilot Mega Magnetometer Library
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#include <AP_Declination.h>
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#include <AP_InertialSensor.h> // ArduPilot Mega Inertial Sensor (accel & gyro) Library
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#include <AP_AHRS.h>
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#include <AP_Airspeed.h>
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#include <AC_PID.h> // PID library
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#include <AC_P.h> // P library
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#include <AP_Buffer.h> // ArduPilot general purpose FIFO buffer
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#include <AP_InertialNav.h> // Inertial Navigation library
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#include <GCS_MAVLink.h>
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#include <AP_Mission.h>
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#include <StorageManager.h>
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#include <AP_Terrain.h>
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#include <AP_Notify.h>
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#include <AP_Vehicle.h>
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#include <DataFlash.h>
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#include <RC_Channel.h> // RC Channel Library
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#include <AP_Motors.h>
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#include <AC_AttitudeControl.h>
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#include <AC_PosControl.h>
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#include <AP_NavEKF.h>
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#include <AP_Nav_Common.h>
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#include <AP_BattMonitor.h>
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const AP_HAL::HAL& hal = AP_HAL_BOARD_DRIVER;
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// key aircraft parameters passed to multiple libraries
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static AP_Vehicle::MultiCopter aparm;
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// INS and Baro declaration
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AP_InertialSensor ins;
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AP_Baro baro;
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#if CONFIG_HAL_BOARD == HAL_BOARD_APM1
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AP_ADC_ADS7844 apm1_adc;
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#endif
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// GPS declaration
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AP_GPS gps;
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GPS_Glitch gps_glitch(gps);
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Baro_Glitch baro_glitch(baro);
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AP_Compass_HMC5843 compass;
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AP_AHRS_DCM ahrs(ins, baro, gps);
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// Inertial Nav declaration
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AP_InertialNav inertial_nav(ahrs, baro, gps_glitch, baro_glitch);
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// fake PIDs
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AC_P p_angle_roll, p_angle_pitch, p_angle_yaw;
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AC_PID pid_rate_roll, pid_rate_pitch, pid_rate_yaw;
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AC_P p_alt_pos, p_pos_xy;
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AC_P pid_alt_rate;
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AC_PID pid_alt_accel;
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AC_PID pid_rate_lat, pid_rate_lon;
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// fake RC inputs
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RC_Channel rc_roll(CH_1), rc_pitch(CH_2), rc_yaw(CH_4), rc_throttle(CH_3);
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// fake motor and outputs
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AP_MotorsQuad motors(rc_roll, rc_pitch, rc_throttle, rc_yaw);
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int16_t motor_roll, motor_pitch, motor_yaw, motor_throttle;
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// Attitude Control
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AC_AttitudeControl ac_control(ahrs, aparm, motors, p_angle_roll, p_angle_pitch, p_angle_yaw, pid_rate_roll, pid_rate_pitch, pid_rate_yaw);
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/// Position Control
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AC_PosControl pos_control(ahrs, inertial_nav, motors, ac_control, p_alt_pos, pid_alt_rate, pid_alt_accel, p_pos_xy, pid_rate_lat, pid_rate_lon);
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void setup()
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{
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hal.console->println("AC_AttitudeControl library test");
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}
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void loop()
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{
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// print message to user
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hal.console->printf_P(PSTR("this example tests compilation only"));
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hal.scheduler->delay(5000);
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}
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AP_HAL_MAIN();
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@ -1 +0,0 @@
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include ../../../../mk/apm.mk
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