mirror of https://github.com/ArduPilot/ardupilot
801 lines
23 KiB
C
801 lines
23 KiB
C
// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
|
|
//
|
|
#ifndef __ARDUCOPTER_CONFIG_H__
|
|
#define __ARDUCOPTER_CONFIG_H__
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
//
|
|
// WARNING WARNING WARNING WARNING WARNING WARNING WARNING WARNING WARNING
|
|
//
|
|
// DO NOT EDIT this file to adjust your configuration. Create your own
|
|
// APM_Config.h and use APM_Config.h.example as a reference.
|
|
//
|
|
// WARNING WARNING WARNING WARNING WARNING WARNING WARNING WARNING WARNING
|
|
///
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
//
|
|
// Default and automatic configuration details.
|
|
//
|
|
// Notes for maintainers:
|
|
//
|
|
// - Try to keep this file organised in the same order as APM_Config.h.example
|
|
//
|
|
#include "defines.h"
|
|
|
|
///
|
|
/// DO NOT EDIT THIS INCLUDE - if you want to make a local change, make that
|
|
/// change in your local copy of APM_Config.h.
|
|
///
|
|
#ifdef USE_CMAKE_APM_CONFIG
|
|
#include "APM_Config_cmake.h" // <== Prefer cmake config if it exists
|
|
#else
|
|
#include "APM_Config.h" // <== THIS INCLUDE, DO NOT EDIT IT. EVER.
|
|
#endif
|
|
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// HARDWARE CONFIGURATION AND CONNECTIONS
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
|
|
#ifdef CONFIG_APM_HARDWARE
|
|
#error CONFIG_APM_HARDWARE option is deprecated! use CONFIG_HAL_BOARD instead
|
|
#endif
|
|
|
|
#ifndef CONFIG_HAL_BOARD
|
|
#error CONFIG_HAL_BOARD must be defined to build ArduCopter
|
|
#endif
|
|
|
|
#ifdef __AVR_ATmega1280__
|
|
#error ATmega1280 is not supported
|
|
#endif
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// FLIGHT CONTROLLER HARDWARE DEFAULT SETTINGS
|
|
//
|
|
#if CONFIG_HAL_BOARD == HAL_BOARD_APM2
|
|
# define CONFIG_IMU_TYPE CONFIG_IMU_MPU6000
|
|
# define CONFIG_SONAR_SOURCE SONAR_SOURCE_ANALOG_PIN
|
|
# define MAGNETOMETER ENABLED
|
|
# define MAIN_LOOP_RATE 100
|
|
# ifdef APM2_BETA_HARDWARE
|
|
# define CONFIG_BARO AP_BARO_BMP085
|
|
# else // APM2 Production Hardware (default)
|
|
# define CONFIG_BARO AP_BARO_MS5611
|
|
# define CONFIG_MS5611_SERIAL AP_BARO_MS5611_SPI
|
|
# endif
|
|
#elif CONFIG_HAL_BOARD == HAL_BOARD_AVR_SITL
|
|
# define CONFIG_IMU_TYPE CONFIG_IMU_SITL
|
|
# define CONFIG_SONAR_SOURCE SONAR_SOURCE_ANALOG_PIN
|
|
# define MAGNETOMETER ENABLED
|
|
# define OPTFLOW DISABLED
|
|
# define MAIN_LOOP_RATE 100
|
|
#elif CONFIG_HAL_BOARD == HAL_BOARD_PX4
|
|
# define CONFIG_IMU_TYPE CONFIG_IMU_PX4
|
|
# define CONFIG_BARO AP_BARO_PX4
|
|
# define CONFIG_SONAR_SOURCE SONAR_SOURCE_ANALOG_PIN
|
|
# define MAGNETOMETER ENABLED
|
|
# define OPTFLOW DISABLED
|
|
# define MAIN_LOOP_RATE 400
|
|
#elif CONFIG_HAL_BOARD == HAL_BOARD_FLYMAPLE
|
|
# define CONFIG_IMU_TYPE CONFIG_IMU_FLYMAPLE
|
|
# define CONFIG_BARO AP_BARO_BMP085
|
|
# define CONFIG_COMPASS AP_COMPASS_HMC5843
|
|
# define CONFIG_ADC DISABLED
|
|
# define MAGNETOMETER ENABLED
|
|
# define CONFIG_SONAR_SOURCE SONAR_SOURCE_ANALOG_PIN
|
|
# define OPTFLOW DISABLED
|
|
# define MAIN_LOOP_RATE 400
|
|
#elif CONFIG_HAL_BOARD == HAL_BOARD_LINUX
|
|
# define CONFIG_IMU_TYPE CONFIG_IMU_L3G4200D
|
|
# define CONFIG_BARO AP_BARO_BMP085
|
|
# define CONFIG_COMPASS AP_COMPASS_HMC5843
|
|
# define CONFIG_ADC DISABLED
|
|
# define MAGNETOMETER ENABLED
|
|
# define CONFIG_SONAR_SOURCE SONAR_SOURCE_ANALOG_PIN
|
|
# define OPTFLOW DISABLED
|
|
# define MAIN_LOOP_RATE 400
|
|
#endif
|
|
|
|
#if MAIN_LOOP_RATE == 400
|
|
# define MAIN_LOOP_SECONDS 0.0025
|
|
# define MAIN_LOOP_MICROS 2500
|
|
#else
|
|
# define MAIN_LOOP_SECONDS 0.01
|
|
# define MAIN_LOOP_MICROS 10000
|
|
#endif
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// FRAME_CONFIG
|
|
//
|
|
#ifndef FRAME_CONFIG
|
|
# define FRAME_CONFIG QUAD_FRAME
|
|
#endif
|
|
|
|
/////////////////////////////////////////////////////////////////////////////////
|
|
// TradHeli defaults
|
|
#if FRAME_CONFIG == HELI_FRAME
|
|
# define RC_FAST_SPEED 125
|
|
# define WP_YAW_BEHAVIOR_DEFAULT WP_YAW_BEHAVIOR_LOOK_AHEAD
|
|
# define RATE_ROLL_D 0
|
|
# define RATE_PITCH_D 0
|
|
# define MPU6K_FILTER 10
|
|
# define HELI_STAB_COLLECTIVE_MIN_DEFAULT 0
|
|
# define HELI_STAB_COLLECTIVE_MAX_DEFAULT 1000
|
|
# define THR_MIN_DEFAULT 0
|
|
# define AUTOTUNE_ENABLED DISABLED
|
|
#endif
|
|
|
|
/////////////////////////////////////////////////////////////////////////////////
|
|
// Y6 defaults
|
|
#if FRAME_CONFIG == Y6_FRAME
|
|
# define RATE_ROLL_P 0.1f
|
|
# define RATE_ROLL_D 0.006f
|
|
# define RATE_PITCH_P 0.1f
|
|
# define RATE_PITCH_D 0.006f
|
|
# define RATE_YAW_P 0.150f
|
|
# define RATE_YAW_I 0.015f
|
|
#endif
|
|
|
|
|
|
// optical flow doesn't work in SITL yet
|
|
#ifdef DESKTOP_BUILD
|
|
# define OPTFLOW DISABLED
|
|
#endif
|
|
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// IMU Selection
|
|
//
|
|
#ifndef CONFIG_IMU_TYPE
|
|
# define CONFIG_IMU_TYPE CONFIG_IMU_OILPAN
|
|
#endif
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// ADC Enable - used to eliminate for systems which don't have ADC.
|
|
//
|
|
#ifndef CONFIG_ADC
|
|
# if CONFIG_IMU_TYPE == CONFIG_IMU_OILPAN
|
|
# define CONFIG_ADC ENABLED
|
|
# else
|
|
# define CONFIG_ADC DISABLED
|
|
# endif
|
|
#endif
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// PWM control
|
|
// default RC speed in Hz
|
|
#ifndef RC_FAST_SPEED
|
|
# define RC_FAST_SPEED 490
|
|
#endif
|
|
|
|
////////////////////////////////////////////////////////
|
|
// LED and IO Pins
|
|
//
|
|
#if CONFIG_HAL_BOARD == HAL_BOARD_APM1
|
|
#elif CONFIG_HAL_BOARD == HAL_BOARD_APM2
|
|
#elif CONFIG_HAL_BOARD == HAL_BOARD_AVR_SITL
|
|
#elif CONFIG_HAL_BOARD == HAL_BOARD_PX4
|
|
#elif CONFIG_HAL_BOARD == HAL_BOARD_FLYMAPLE
|
|
#elif CONFIG_HAL_BOARD == HAL_BOARD_LINUX
|
|
# define LED_ON LOW
|
|
# define LED_OFF HIGH
|
|
#endif
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// Barometer
|
|
//
|
|
|
|
#ifndef CONFIG_BARO
|
|
# define CONFIG_BARO AP_BARO_BMP085
|
|
#endif
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// Sonar
|
|
//
|
|
|
|
#ifndef CONFIG_SONAR_SOURCE
|
|
# define CONFIG_SONAR_SOURCE SONAR_SOURCE_ADC
|
|
#endif
|
|
|
|
#if CONFIG_SONAR_SOURCE == SONAR_SOURCE_ADC && CONFIG_ADC == DISABLED
|
|
# warning Cannot use ADC for CONFIG_SONAR_SOURCE, becaude CONFIG_ADC is DISABLED
|
|
# warning Defaulting CONFIG_SONAR_SOURCE to ANALOG_PIN
|
|
# undef CONFIG_SONAR_SOURCE
|
|
# define CONFIG_SONAR_SOURCE SONAR_SOURCE_ANALOG_PIN
|
|
#endif
|
|
|
|
#if CONFIG_SONAR_SOURCE == SONAR_SOURCE_ADC
|
|
# ifndef CONFIG_SONAR_SOURCE_ADC_CHANNEL
|
|
# define CONFIG_SONAR_SOURCE_ADC_CHANNEL 7
|
|
# endif
|
|
#elif CONFIG_SONAR_SOURCE == SONAR_SOURCE_ANALOG_PIN
|
|
# ifndef CONFIG_SONAR_SOURCE_ANALOG_PIN
|
|
# define CONFIG_SONAR_SOURCE_ANALOG_PIN 0
|
|
# endif
|
|
#else
|
|
# warning Invalid value for CONFIG_SONAR_SOURCE, disabling sonar
|
|
# define CONFIG_SONAR DISABLED
|
|
#endif
|
|
|
|
#ifndef CONFIG_SONAR
|
|
# define CONFIG_SONAR ENABLED
|
|
#endif
|
|
|
|
#ifndef SONAR_ALT_HEALTH_MAX
|
|
# define SONAR_ALT_HEALTH_MAX 3 // number of good reads that indicates a healthy sonar
|
|
#endif
|
|
|
|
#ifndef SONAR_RELIABLE_DISTANCE_PCT
|
|
# define SONAR_RELIABLE_DISTANCE_PCT 0.60f // we trust the sonar out to 60% of it's maximum range
|
|
#endif
|
|
|
|
#ifndef SONAR_GAIN_DEFAULT
|
|
# define SONAR_GAIN_DEFAULT 0.8 // gain for controlling how quickly sonar range adjusts target altitude (lower means slower reaction)
|
|
#endif
|
|
|
|
#ifndef THR_SURFACE_TRACKING_VELZ_MAX
|
|
# define THR_SURFACE_TRACKING_VELZ_MAX 150 // max vertical speed change while surface tracking with sonar
|
|
#endif
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// Channel 7 and 8 default options
|
|
//
|
|
|
|
#ifndef CH7_OPTION
|
|
# define CH7_OPTION AUX_SWITCH_DO_NOTHING
|
|
#endif
|
|
|
|
#ifndef CH8_OPTION
|
|
# define CH8_OPTION AUX_SWITCH_DO_NOTHING
|
|
#endif
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// HIL_MODE OPTIONAL
|
|
|
|
#ifndef HIL_MODE
|
|
#define HIL_MODE HIL_MODE_DISABLED
|
|
#endif
|
|
|
|
#if HIL_MODE != HIL_MODE_DISABLED // we are in HIL mode
|
|
|
|
# undef GPS_PROTOCOL
|
|
# define GPS_PROTOCOL GPS_PROTOCOL_NONE
|
|
|
|
#undef CONFIG_SONAR
|
|
#define CONFIG_SONAR DISABLED
|
|
#endif
|
|
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// GPS_PROTOCOL
|
|
//
|
|
#ifndef GPS_PROTOCOL
|
|
# define GPS_PROTOCOL GPS_PROTOCOL_AUTO
|
|
#endif
|
|
|
|
|
|
#ifndef MAV_SYSTEM_ID
|
|
# define MAV_SYSTEM_ID 1
|
|
#endif
|
|
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// Serial port speeds.
|
|
//
|
|
#ifndef SERIAL0_BAUD
|
|
# define SERIAL0_BAUD 115200
|
|
#endif
|
|
#ifndef SERIAL1_BAUD
|
|
# define SERIAL1_BAUD 57600
|
|
#endif
|
|
#ifndef SERIAL2_BAUD
|
|
# define SERIAL2_BAUD 57600
|
|
#endif
|
|
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// Battery monitoring
|
|
//
|
|
#ifndef FS_BATT_VOLTAGE_DEFAULT
|
|
# define FS_BATT_VOLTAGE_DEFAULT 10.5f // default battery voltage below which failsafe will be triggered
|
|
#endif
|
|
|
|
#ifndef FS_BATT_MAH_DEFAULT
|
|
# define FS_BATT_MAH_DEFAULT 0 // default battery capacity (in mah) below which failsafe will be triggered
|
|
#endif
|
|
|
|
#ifndef BOARD_VOLTAGE_MIN
|
|
# define BOARD_VOLTAGE_MIN 4.3f // min board voltage in volts for pre-arm checks
|
|
#endif
|
|
|
|
#ifndef BOARD_VOLTAGE_MAX
|
|
# define BOARD_VOLTAGE_MAX 5.8f // max board voltage in volts for pre-arm checks
|
|
#endif
|
|
|
|
// GPS failsafe
|
|
#ifndef FAILSAFE_GPS_TIMEOUT_MS
|
|
# define FAILSAFE_GPS_TIMEOUT_MS 5000 // gps failsafe triggers after 5 seconds with no GPS
|
|
#endif
|
|
#ifndef GPS_HDOP_GOOD_DEFAULT
|
|
# define GPS_HDOP_GOOD_DEFAULT 200 // minimum hdop that represents a good position. used during pre-arm checks if fence is enabled
|
|
#endif
|
|
|
|
// GCS failsafe
|
|
#ifndef FS_GCS
|
|
# define FS_GCS DISABLED
|
|
#endif
|
|
#ifndef FS_GCS_TIMEOUT_MS
|
|
# define FS_GCS_TIMEOUT_MS 5000 // gcs failsafe triggers after 5 seconds with no GCS heartbeat
|
|
#endif
|
|
// possible values for FS_GCS parameter
|
|
#define FS_GCS_DISABLED 0
|
|
#define FS_GCS_ENABLED_ALWAYS_RTL 1
|
|
#define FS_GCS_ENABLED_CONTINUE_MISSION 2
|
|
|
|
// pre-arm check max velocity
|
|
#ifndef PREARM_MAX_VELOCITY_CMS
|
|
# define PREARM_MAX_VELOCITY_CMS 50.0f // vehicle must be travelling under 50cm/s before arming
|
|
#endif
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// MAGNETOMETER
|
|
#ifndef MAGNETOMETER
|
|
# define MAGNETOMETER ENABLED
|
|
#endif
|
|
|
|
// expected magnetic field strength. pre-arm checks will fail if 50% higher or lower than this value
|
|
#if CONFIG_HAL_BOARD == HAL_BOARD_APM1 || CONFIG_HAL_BOARD == HAL_BOARD_APM2
|
|
#ifndef COMPASS_MAGFIELD_EXPECTED
|
|
# define COMPASS_MAGFIELD_EXPECTED 330 // pre arm will fail if mag field > 544 or < 115
|
|
#endif
|
|
#else // PX4, SITL
|
|
#ifndef COMPASS_MAGFIELD_EXPECTED
|
|
#define COMPASS_MAGFIELD_EXPECTED 530 // pre arm will fail if mag field > 874 or < 185
|
|
#endif
|
|
#endif
|
|
|
|
// max compass offset length (i.e. sqrt(offs_x^2+offs_y^2+offs_Z^2))
|
|
#ifndef CONFIG_ARCH_BOARD_PX4FMU_V1
|
|
#ifndef COMPASS_OFFSETS_MAX
|
|
# define COMPASS_OFFSETS_MAX 600 // PX4 onboard compass has high offsets
|
|
#endif
|
|
#else // APM1, APM2, SITL, FLYMAPLE, etc
|
|
#ifndef COMPASS_OFFSETS_MAX
|
|
# define COMPASS_OFFSETS_MAX 500
|
|
#endif
|
|
#endif
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// OPTICAL_FLOW
|
|
#ifndef OPTFLOW // sets global enabled/disabled flag for optflow (as seen in CLI)
|
|
# define OPTFLOW ENABLED
|
|
#endif
|
|
// optical flow based loiter PI values
|
|
#ifndef OPTFLOW_ROLL_P
|
|
#define OPTFLOW_ROLL_P 2.5f
|
|
#endif
|
|
#ifndef OPTFLOW_ROLL_I
|
|
#define OPTFLOW_ROLL_I 0.5f
|
|
#endif
|
|
#ifndef OPTFLOW_ROLL_D
|
|
#define OPTFLOW_ROLL_D 0.12f
|
|
#endif
|
|
#ifndef OPTFLOW_PITCH_P
|
|
#define OPTFLOW_PITCH_P 2.5f
|
|
#endif
|
|
#ifndef OPTFLOW_PITCH_I
|
|
#define OPTFLOW_PITCH_I 0.5f
|
|
#endif
|
|
#ifndef OPTFLOW_PITCH_D
|
|
#define OPTFLOW_PITCH_D 0.12f
|
|
#endif
|
|
#ifndef OPTFLOW_IMAX
|
|
#define OPTFLOW_IMAX 100
|
|
#endif
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// Auto Tuning
|
|
#ifndef AUTOTUNE_ENABLED
|
|
# define AUTOTUNE_ENABLED ENABLED
|
|
#endif
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// Crop Sprayer
|
|
#ifndef SPRAYER
|
|
# define SPRAYER DISABLED
|
|
#endif
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// EPM cargo gripper
|
|
#ifndef EPM_ENABLED
|
|
# define EPM_ENABLED DISABLED
|
|
#endif
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// RADIO CONFIGURATION
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// FLIGHT_MODE
|
|
//
|
|
|
|
#if !defined(FLIGHT_MODE_1)
|
|
# define FLIGHT_MODE_1 STABILIZE
|
|
#endif
|
|
#if !defined(FLIGHT_MODE_2)
|
|
# define FLIGHT_MODE_2 STABILIZE
|
|
#endif
|
|
#if !defined(FLIGHT_MODE_3)
|
|
# define FLIGHT_MODE_3 STABILIZE
|
|
#endif
|
|
#if !defined(FLIGHT_MODE_4)
|
|
# define FLIGHT_MODE_4 STABILIZE
|
|
#endif
|
|
#if !defined(FLIGHT_MODE_5)
|
|
# define FLIGHT_MODE_5 STABILIZE
|
|
#endif
|
|
#if !defined(FLIGHT_MODE_6)
|
|
# define FLIGHT_MODE_6 STABILIZE
|
|
#endif
|
|
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// Throttle Failsafe
|
|
//
|
|
#ifndef FS_THR_VALUE_DEFAULT
|
|
# define FS_THR_VALUE_DEFAULT 975
|
|
#endif
|
|
|
|
#ifndef LAND_SPEED
|
|
# define LAND_SPEED 50 // the descent speed for the final stage of landing in cm/s
|
|
#endif
|
|
#ifndef LAND_START_ALT
|
|
# define LAND_START_ALT 1000 // altitude in cm where land controller switches to slow rate of descent
|
|
#endif
|
|
#ifndef LAND_DETECTOR_TRIGGER
|
|
# define LAND_DETECTOR_TRIGGER 50 // number of 50hz iterations with near zero climb rate and low throttle that triggers landing complete.
|
|
#endif
|
|
#ifndef LAND_REQUIRE_MIN_THROTTLE_TO_DISARM // require pilot to reduce throttle to minimum before vehicle will disarm
|
|
# define LAND_REQUIRE_MIN_THROTTLE_TO_DISARM ENABLED
|
|
#endif
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// CAMERA TRIGGER AND CONTROL
|
|
//
|
|
#ifndef CAMERA
|
|
# define CAMERA ENABLED
|
|
#endif
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// MOUNT (ANTENNA OR CAMERA)
|
|
//
|
|
#ifndef MOUNT
|
|
# define MOUNT ENABLED
|
|
#endif
|
|
|
|
#ifndef MOUNT2
|
|
# define MOUNT2 DISABLED
|
|
#endif
|
|
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// Flight mode definitions
|
|
//
|
|
|
|
// Acro Mode
|
|
#ifndef ACRO_RP_P
|
|
# define ACRO_RP_P 4.5f
|
|
#endif
|
|
|
|
#ifndef ACRO_YAW_P
|
|
# define ACRO_YAW_P 4.5f
|
|
#endif
|
|
|
|
#ifndef ACRO_LEVEL_MAX_ANGLE
|
|
# define ACRO_LEVEL_MAX_ANGLE 3000
|
|
#endif
|
|
|
|
#ifndef ACRO_BALANCE_ROLL
|
|
#define ACRO_BALANCE_ROLL 1.0f
|
|
#endif
|
|
|
|
#ifndef ACRO_BALANCE_PITCH
|
|
#define ACRO_BALANCE_PITCH 1.0f
|
|
#endif
|
|
|
|
// Stabilize (angle controller) gains
|
|
#ifndef STABILIZE_ROLL_P
|
|
# define STABILIZE_ROLL_P 4.5f
|
|
#endif
|
|
#ifndef STABILIZE_ROLL_I
|
|
# define STABILIZE_ROLL_I 0.0f
|
|
#endif
|
|
#ifndef STABILIZE_ROLL_IMAX
|
|
# define STABILIZE_ROLL_IMAX 0
|
|
#endif
|
|
|
|
#ifndef STABILIZE_PITCH_P
|
|
# define STABILIZE_PITCH_P 4.5f
|
|
#endif
|
|
#ifndef STABILIZE_PITCH_I
|
|
# define STABILIZE_PITCH_I 0.0f
|
|
#endif
|
|
#ifndef STABILIZE_PITCH_IMAX
|
|
# define STABILIZE_PITCH_IMAX 0
|
|
#endif
|
|
|
|
#ifndef STABILIZE_YAW_P
|
|
# define STABILIZE_YAW_P 4.5f
|
|
#endif
|
|
#ifndef STABILIZE_YAW_I
|
|
# define STABILIZE_YAW_I 0.0f
|
|
#endif
|
|
#ifndef STABILIZE_YAW_IMAX
|
|
# define STABILIZE_YAW_IMAX 0
|
|
#endif
|
|
|
|
// RTL Mode
|
|
#ifndef RTL_ALT_FINAL
|
|
# define RTL_ALT_FINAL 0 // the altitude the vehicle will move to as the final stage of Returning to Launch. Set to zero to land.
|
|
#endif
|
|
|
|
#ifndef RTL_ALT
|
|
# define RTL_ALT 1500 // default alt to return to home in cm, 0 = Maintain current altitude
|
|
#endif
|
|
|
|
#ifndef RTL_ALT_MAX
|
|
# define RTL_ALT_MAX 8000 // Max height to return to home in cm (i.e 80m)
|
|
#endif
|
|
|
|
#ifndef RTL_LOITER_TIME
|
|
# define RTL_LOITER_TIME 5000 // Time (in milliseconds) to loiter above home before begining final descent
|
|
#endif
|
|
|
|
// AUTO Mode
|
|
#ifndef WP_YAW_BEHAVIOR_DEFAULT
|
|
# define WP_YAW_BEHAVIOR_DEFAULT WP_YAW_BEHAVIOR_LOOK_AT_NEXT_WP_EXCEPT_RTL
|
|
#endif
|
|
|
|
#ifndef AUTO_YAW_SLEW_RATE
|
|
# define AUTO_YAW_SLEW_RATE 60 // degrees/sec
|
|
#endif
|
|
|
|
#ifndef YAW_LOOK_AHEAD_MIN_SPEED
|
|
# define YAW_LOOK_AHEAD_MIN_SPEED 100 // minimum ground speed in cm/s required before copter is aimed at ground course
|
|
#endif
|
|
|
|
// Super Simple mode
|
|
#ifndef SUPER_SIMPLE_RADIUS
|
|
# define SUPER_SIMPLE_RADIUS 1000
|
|
#endif
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// Stabilize Rate Control
|
|
//
|
|
#ifndef ROLL_PITCH_INPUT_MAX
|
|
# define ROLL_PITCH_INPUT_MAX 4500 // roll, pitch input range
|
|
#endif
|
|
#ifndef DEFAULT_ANGLE_MAX
|
|
# define DEFAULT_ANGLE_MAX 4500 // ANGLE_MAX parameters default value
|
|
#endif
|
|
#ifndef ANGLE_RATE_MAX
|
|
# define ANGLE_RATE_MAX 18000 // default maximum rotation rate in roll/pitch axis requested by angle controller used in stabilize, loiter, rtl, auto flight modes
|
|
#endif
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// Rate controller gains
|
|
//
|
|
#ifndef RATE_ROLL_P
|
|
# define RATE_ROLL_P 0.150f
|
|
#endif
|
|
#ifndef RATE_ROLL_I
|
|
# define RATE_ROLL_I 0.100f
|
|
#endif
|
|
#ifndef RATE_ROLL_D
|
|
# define RATE_ROLL_D 0.004f
|
|
#endif
|
|
#ifndef RATE_ROLL_IMAX
|
|
# define RATE_ROLL_IMAX 500
|
|
#endif
|
|
|
|
#ifndef RATE_PITCH_P
|
|
# define RATE_PITCH_P 0.150f
|
|
#endif
|
|
#ifndef RATE_PITCH_I
|
|
# define RATE_PITCH_I 0.100f
|
|
#endif
|
|
#ifndef RATE_PITCH_D
|
|
# define RATE_PITCH_D 0.004f
|
|
#endif
|
|
#ifndef RATE_PITCH_IMAX
|
|
# define RATE_PITCH_IMAX 500
|
|
#endif
|
|
|
|
#ifndef RATE_YAW_P
|
|
# define RATE_YAW_P 0.200f
|
|
#endif
|
|
#ifndef RATE_YAW_I
|
|
# define RATE_YAW_I 0.020f
|
|
#endif
|
|
#ifndef RATE_YAW_D
|
|
# define RATE_YAW_D 0.000f
|
|
#endif
|
|
#ifndef RATE_YAW_IMAX
|
|
# define RATE_YAW_IMAX 800
|
|
#endif
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// Loiter position control gains
|
|
//
|
|
#ifndef LOITER_P
|
|
# define LOITER_P 1.0f
|
|
#endif
|
|
#ifndef LOITER_I
|
|
# define LOITER_I 0.0f
|
|
#endif
|
|
#ifndef LOITER_IMAX
|
|
# define LOITER_IMAX 0
|
|
#endif
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// Loiter rate control gains
|
|
//
|
|
#ifndef LOITER_RATE_P
|
|
# define LOITER_RATE_P 1.0f
|
|
#endif
|
|
#ifndef LOITER_RATE_I
|
|
# define LOITER_RATE_I 0.5f
|
|
#endif
|
|
#ifndef LOITER_RATE_D
|
|
# define LOITER_RATE_D 0.0f
|
|
#endif
|
|
#ifndef LOITER_RATE_IMAX
|
|
# define LOITER_RATE_IMAX 400 // maximum acceleration from I term build-up in cm/s/s
|
|
#endif
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// Throttle control gains
|
|
//
|
|
#ifndef THROTTLE_CRUISE
|
|
# define THROTTLE_CRUISE 450 // default estimate of throttle required for vehicle to maintain a hover
|
|
#endif
|
|
|
|
#ifndef THR_MID_DEFAULT
|
|
# define THR_MID_DEFAULT 500 // Throttle output (0 ~ 1000) when throttle stick is in mid position
|
|
#endif
|
|
|
|
#ifndef THR_MIN_DEFAULT
|
|
# define THR_MIN_DEFAULT 130 // minimum throttle sent to the motors when armed and pilot throttle above zero
|
|
#endif
|
|
#ifndef THR_MAX_DEFAULT
|
|
# define THR_MAX_DEFAULT 1000 // maximum throttle sent to the motors
|
|
#endif
|
|
|
|
#ifndef THROTTLE_IN_DEADBAND
|
|
# define THROTTLE_IN_DEADBAND 100 // the throttle input channel's deadband in PWM
|
|
#endif
|
|
|
|
#ifndef ALT_HOLD_P
|
|
# define ALT_HOLD_P 1.0f
|
|
#endif
|
|
#ifndef ALT_HOLD_I
|
|
# define ALT_HOLD_I 0.0f
|
|
#endif
|
|
#ifndef ALT_HOLD_IMAX
|
|
# define ALT_HOLD_IMAX 300
|
|
#endif
|
|
|
|
// RATE control
|
|
#ifndef THROTTLE_RATE_P
|
|
# define THROTTLE_RATE_P 6.0f
|
|
#endif
|
|
#ifndef THROTTLE_RATE_I
|
|
# define THROTTLE_RATE_I 0.0f
|
|
#endif
|
|
#ifndef THROTTLE_RATE_D
|
|
# define THROTTLE_RATE_D 0.0f
|
|
#endif
|
|
|
|
#ifndef THROTTLE_RATE_IMAX
|
|
# define THROTTLE_RATE_IMAX 300
|
|
#endif
|
|
|
|
// default maximum vertical velocity the pilot may request
|
|
#ifndef PILOT_VELZ_MAX
|
|
# define PILOT_VELZ_MAX 250 // maximum vertical velocity in cm/s
|
|
#endif
|
|
|
|
// max distance in cm above or below current location that will be used for the alt target when transitioning to alt-hold mode
|
|
#ifndef ALT_HOLD_INIT_MAX_OVERSHOOT
|
|
# define ALT_HOLD_INIT_MAX_OVERSHOOT 200
|
|
#endif
|
|
// the acceleration used to define the distance-velocity curve
|
|
#ifndef ALT_HOLD_ACCEL_MAX
|
|
# define ALT_HOLD_ACCEL_MAX 250 // if you change this you must also update the duplicate declaration in AC_WPNav.h
|
|
#endif
|
|
|
|
// Throttle Accel control
|
|
#ifndef THROTTLE_ACCEL_P
|
|
# define THROTTLE_ACCEL_P 0.75f
|
|
#endif
|
|
#ifndef THROTTLE_ACCEL_I
|
|
# define THROTTLE_ACCEL_I 1.50f
|
|
#endif
|
|
#ifndef THROTTLE_ACCEL_D
|
|
# define THROTTLE_ACCEL_D 0.0f
|
|
#endif
|
|
#ifndef THROTTLE_ACCEL_IMAX
|
|
# define THROTTLE_ACCEL_IMAX 500
|
|
#endif
|
|
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// Dataflash logging control
|
|
//
|
|
#ifndef LOGGING_ENABLED
|
|
# define LOGGING_ENABLED ENABLED
|
|
#endif
|
|
|
|
#if CONFIG_HAL_BOARD == HAL_BOARD_APM1 || CONFIG_HAL_BOARD == HAL_BOARD_APM2 || CONFIG_HAL_BOARD == HAL_BOARD_AVR_SITL
|
|
// APM1 & APM2 default logging
|
|
# define DEFAULT_LOG_BITMASK \
|
|
MASK_LOG_ATTITUDE_MED | \
|
|
MASK_LOG_GPS | \
|
|
MASK_LOG_PM | \
|
|
MASK_LOG_CTUN | \
|
|
MASK_LOG_NTUN | \
|
|
MASK_LOG_RCIN | \
|
|
MASK_LOG_CMD | \
|
|
MASK_LOG_CURRENT
|
|
#else
|
|
// PX4, Pixhawk, FlyMaple default logging
|
|
# define DEFAULT_LOG_BITMASK \
|
|
MASK_LOG_ATTITUDE_MED | \
|
|
MASK_LOG_GPS | \
|
|
MASK_LOG_PM | \
|
|
MASK_LOG_CTUN | \
|
|
MASK_LOG_NTUN | \
|
|
MASK_LOG_RCIN | \
|
|
MASK_LOG_IMU | \
|
|
MASK_LOG_CMD | \
|
|
MASK_LOG_CURRENT | \
|
|
MASK_LOG_RCOUT | \
|
|
MASK_LOG_COMPASS | \
|
|
MASK_LOG_CAMERA
|
|
#endif
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// AP_Limits Defaults
|
|
//
|
|
|
|
// Enable/disable AP_Limits
|
|
#ifndef AC_FENCE
|
|
#define AC_FENCE ENABLED
|
|
#endif
|
|
|
|
|
|
//////////////////////////////////////////////////////////////////////////////
|
|
// Developer Items
|
|
//
|
|
|
|
// use this to completely disable the CLI
|
|
#ifndef CLI_ENABLED
|
|
# define CLI_ENABLED ENABLED
|
|
#endif
|
|
|
|
/*
|
|
build a firmware version string.
|
|
GIT_VERSION comes from Makefile builds
|
|
*/
|
|
#ifndef GIT_VERSION
|
|
#define FIRMWARE_STRING THISFIRMWARE
|
|
#else
|
|
#define FIRMWARE_STRING THISFIRMWARE " (" GIT_VERSION ")"
|
|
#endif
|
|
|
|
#endif // __ARDUCOPTER_CONFIG_H__
|