mirror of https://github.com/ArduPilot/ardupilot
438 lines
19 KiB
C
438 lines
19 KiB
C
// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
|
|
|
|
#ifndef _DEFINES_H
|
|
#define _DEFINES_H
|
|
|
|
#include <AP_HAL_Boards.h>
|
|
|
|
// Just so that it's completely clear...
|
|
#define ENABLED 1
|
|
#define DISABLED 0
|
|
|
|
// this avoids a very common config error
|
|
#define ENABLE ENABLED
|
|
#define DISABLE DISABLED
|
|
|
|
// Flight modes
|
|
// ------------
|
|
#define YAW_HOLD 0 // heading hold at heading in nav_yaw but allow input from pilot
|
|
#define YAW_ACRO 1 // pilot controlled yaw using rate controller
|
|
#define YAW_LOOK_AT_NEXT_WP 2 // point towards next waypoint (no pilot input accepted)
|
|
#define YAW_LOOK_AT_LOCATION 3 // point towards a location held in yaw_look_at_WP (no pilot input accepted)
|
|
#define YAW_CIRCLE 4 // point towards a location held in yaw_look_at_WP (no pilot input accepted)
|
|
#define YAW_LOOK_AT_HOME 5 // point towards home (no pilot input accepted)
|
|
#define YAW_LOOK_AT_HEADING 6 // point towards a particular angle (not pilot input accepted)
|
|
#define YAW_LOOK_AHEAD 7 // WARNING! CODE IN DEVELOPMENT NOT PROVEN
|
|
#define YAW_TOY 8 // THOR This is the Yaw mode
|
|
#define YAW_RESETTOARMEDYAW 9 // point towards heading at time motors were armed
|
|
|
|
#define ROLL_PITCH_STABLE 0 // pilot input roll, pitch angles
|
|
#define ROLL_PITCH_ACRO 1 // pilot inputs roll, pitch rotation rates
|
|
#define ROLL_PITCH_AUTO 2 // no pilot input. autopilot roll, pitch is sent to stabilize controller inputs
|
|
#define ROLL_PITCH_STABLE_OF 3 // pilot inputs roll, pitch angles which are mixed with optical flow based position controller lean anbles
|
|
#define ROLL_PITCH_TOY 4 // THOR This is the Roll and Pitch mode
|
|
#define ROLL_PITCH_LOITER 5 // pilot inputs the desired horizontal velocities
|
|
|
|
#define THROTTLE_MANUAL 0 // manual throttle mode - pilot input goes directly to motors
|
|
#define THROTTLE_MANUAL_TILT_COMPENSATED 1 // mostly manual throttle but with some tilt compensation
|
|
#define THROTTLE_HOLD 2 // alt hold plus pilot input of climb rate
|
|
#define THROTTLE_AUTO 3 // auto pilot altitude controller with target altitude held in next_WP.alt
|
|
#define THROTTLE_LAND 4 // landing throttle controller
|
|
|
|
|
|
// sonar - for use with CONFIG_SONAR_SOURCE
|
|
#define SONAR_SOURCE_ADC 1
|
|
#define SONAR_SOURCE_ANALOG_PIN 2
|
|
|
|
// Ch7 and Ch8 aux switch control
|
|
#define AUX_SWITCH_PWM_TRIGGER 1800 // pwm value above which the ch7 or ch8 option will be invoked
|
|
#define CH6_PWM_TRIGGER_HIGH 1800
|
|
#define CH6_PWM_TRIGGER_LOW 1200
|
|
|
|
#define AUX_SWITCH_DO_NOTHING 0 // aux switch disabled
|
|
#define AUX_SWITCH_SET_HOVER 1 // deprecated
|
|
#define AUX_SWITCH_FLIP 2 // flip
|
|
#define AUX_SWITCH_SIMPLE_MODE 3 // change to simple mode
|
|
#define AUX_SWITCH_RTL 4 // change to RTL flight mode
|
|
#define AUX_SWITCH_SAVE_TRIM 5 // save current position as level
|
|
#define AUX_SWITCH_ADC_FILTER 6 // deprecated
|
|
#define AUX_SWITCH_SAVE_WP 7 // save mission waypoint or RTL if in auto mode
|
|
#define AUX_SWITCH_MULTI_MODE 8 // depending upon CH6 position Flip (if ch6 is low), RTL (if ch6 in middle) or Save WP (if ch6 is high)
|
|
#define AUX_SWITCH_CAMERA_TRIGGER 9 // trigger camera servo or relay
|
|
#define AUX_SWITCH_SONAR 10 // allow enabling or disabling sonar in flight which helps avoid surface tracking when you are far above the ground
|
|
#define AUX_SWITCH_FENCE 11 // allow enabling or disabling fence in flight
|
|
#define AUX_SWITCH_RESETTOARMEDYAW 12 // changes yaw to be same as when quad was armed
|
|
|
|
|
|
// Frame types
|
|
#define QUAD_FRAME 0
|
|
#define TRI_FRAME 1
|
|
#define HEXA_FRAME 2
|
|
#define Y6_FRAME 3
|
|
#define OCTA_FRAME 4
|
|
#define HELI_FRAME 5
|
|
#define OCTA_QUAD_FRAME 6
|
|
|
|
#define PLUS_FRAME 0
|
|
#define X_FRAME 1
|
|
#define V_FRAME 2
|
|
|
|
// LED output
|
|
#define NORMAL_LEDS 0
|
|
#define SAVE_TRIM_LEDS 1
|
|
|
|
|
|
// Internal defines, don't edit and expect things to work
|
|
// -------------------------------------------------------
|
|
|
|
#define TRUE 1
|
|
#define FALSE 0
|
|
#define ToRad(x) radians(x) // *pi/180
|
|
#define ToDeg(x) degrees(x) // *180/pi
|
|
|
|
#define DEBUG 0
|
|
#define LOITER_RANGE 60 // for calculating power outside of loiter radius
|
|
|
|
#define T6 1000000
|
|
#define T7 10000000
|
|
|
|
// GPS type codes - use the names, not the numbers
|
|
#define GPS_PROTOCOL_NONE -1
|
|
#define GPS_PROTOCOL_NMEA 0
|
|
#define GPS_PROTOCOL_SIRF 1
|
|
#define GPS_PROTOCOL_UBLOX 2
|
|
#define GPS_PROTOCOL_IMU 3
|
|
#define GPS_PROTOCOL_MTK 4
|
|
#define GPS_PROTOCOL_HIL 5
|
|
#define GPS_PROTOCOL_MTK19 6
|
|
#define GPS_PROTOCOL_AUTO 7
|
|
|
|
// HIL enumerations
|
|
#define HIL_MODE_DISABLED 0
|
|
#define HIL_MODE_ATTITUDE 1
|
|
#define HIL_MODE_SENSORS 2
|
|
|
|
// Altitude status definitions
|
|
#define REACHED_ALT 0
|
|
#define DESCENDING 1
|
|
#define ASCENDING 2
|
|
|
|
// Auto Pilot modes
|
|
// ----------------
|
|
#define STABILIZE 0 // hold level position
|
|
#define ACRO 1 // rate control
|
|
#define ALT_HOLD 2 // AUTO control
|
|
#define AUTO 3 // AUTO control
|
|
#define GUIDED 4 // AUTO control
|
|
#define LOITER 5 // Hold a single location
|
|
#define RTL 6 // AUTO control
|
|
#define CIRCLE 7 // AUTO control
|
|
#define POSITION 8 // AUTO control
|
|
#define LAND 9 // AUTO control
|
|
#define OF_LOITER 10 // Hold a single location using optical flow
|
|
// sensor
|
|
#define TOY_A 11 // THOR Enum for Toy mode
|
|
#define TOY_M 12 // THOR Enum for Toy mode
|
|
#define NUM_MODES 13
|
|
|
|
// CH_6 Tuning
|
|
// -----------
|
|
#define CH6_NONE 0 // no tuning performed
|
|
#define CH6_STABILIZE_KP 1 // stabilize roll/pitch angle controller's P term
|
|
#define CH6_STABILIZE_KI 2 // stabilize roll/pitch angle controller's I term
|
|
#define CH6_STABILIZE_KD 29 // stabilize roll/pitch angle controller's D term
|
|
#define CH6_YAW_KP 3 // stabilize yaw heading controller's P term
|
|
#define CH6_YAW_KI 24 // stabilize yaw heading controller's P term
|
|
#define CH6_ACRO_KP 25 // acro controller's P term. converts pilot input to a desired roll, pitch or yaw rate
|
|
#define CH6_RATE_KP 4 // body frame roll/pitch rate controller's P term
|
|
#define CH6_RATE_KI 5 // body frame roll/pitch rate controller's I term
|
|
#define CH6_RATE_KD 21 // body frame roll/pitch rate controller's D term
|
|
#define CH6_YAW_RATE_KP 6 // body frame yaw rate controller's P term
|
|
#define CH6_YAW_RATE_KD 26 // body frame yaw rate controller's D term
|
|
#define CH6_THR_HOLD_KP 14 // altitude hold controller's P term (alt error to desired rate)
|
|
#define CH6_THROTTLE_KP 7 // throttle rate controller's P term (desired rate to acceleration or motor output)
|
|
#define CH6_THROTTLE_KI 33 // throttle rate controller's I term (desired rate to acceleration or motor output)
|
|
#define CH6_THROTTLE_KD 37 // throttle rate controller's D term (desired rate to acceleration or motor output)
|
|
#define CH6_THR_ACCEL_KP 34 // accel based throttle controller's P term
|
|
#define CH6_THR_ACCEL_KI 35 // accel based throttle controller's I term
|
|
#define CH6_THR_ACCEL_KD 36 // accel based throttle controller's D term
|
|
#define CH6_RELAY 9 // switch relay on if ch6 high, off if low
|
|
#define CH6_WP_SPEED 10 // maximum speed to next way point (0 to 10m/s)
|
|
#define CH6_LOITER_KP 12 // loiter distance controller's P term (position error to speed)
|
|
#define CH6_LOITER_KI 27 // loiter distance controller's I term (position error to speed)
|
|
#define CH6_HELI_EXTERNAL_GYRO 13 // TradHeli specific external tail gyro gain
|
|
#define CH6_OPTFLOW_KP 17 // optical flow loiter controller's P term (position error to tilt angle)
|
|
#define CH6_OPTFLOW_KI 18 // optical flow loiter controller's I term (position error to tilt angle)
|
|
#define CH6_OPTFLOW_KD 19 // optical flow loiter controller's D term (position error to tilt angle)
|
|
#define CH6_LOITER_RATE_KP 22 // loiter rate controller's P term (speed error to tilt angle)
|
|
#define CH6_LOITER_RATE_KI 28 // loiter rate controller's I term (speed error to tilt angle)
|
|
#define CH6_LOITER_RATE_KD 23 // loiter rate controller's D term (speed error to tilt angle)
|
|
#define CH6_AHRS_YAW_KP 30 // ahrs's compass effect on yaw angle (0 = very low, 1 = very high)
|
|
#define CH6_AHRS_KP 31 // accelerometer effect on roll/pitch angle (0=low)
|
|
#define CH6_INAV_TC 32 // inertial navigation baro/accel and gps/accel time constant (1.5 = strong baro/gps correction on accel estimatehas very strong does not correct accel estimate, 7 = very weak correction)
|
|
#define CH6_DECLINATION 38 // compass declination in radians
|
|
#define CH6_CIRCLE_RATE 39 // circle turn rate in degrees (hard coded to about 45 degrees in either direction)
|
|
|
|
|
|
// Commands - Note that APM now uses a subset of the MAVLink protocol
|
|
// commands. See enum MAV_CMD in the GCS_Mavlink library
|
|
#define CMD_BLANK 0 // there is no command stored in the mem location
|
|
// requested
|
|
#define NO_COMMAND 0
|
|
|
|
|
|
// Navigation modes held in nav_mode variable
|
|
#define NAV_NONE 0
|
|
#define NAV_CIRCLE 1
|
|
#define NAV_LOITER 2
|
|
#define NAV_WP 3
|
|
|
|
// Yaw behaviours during missions - possible values for WP_YAW_BEHAVIOR parameter
|
|
#define WP_YAW_BEHAVIOR_NONE 0 // auto pilot will never control yaw during missions or rtl (except for DO_CONDITIONAL_YAW command received)
|
|
#define WP_YAW_BEHAVIOR_LOOK_AT_NEXT_WP 1 // auto pilot will face next waypoint or home during rtl
|
|
#define WP_YAW_BEHAVIOR_LOOK_AT_NEXT_WP_EXCEPT_RTL 2 // auto pilot will face next waypoint except when doing RTL at which time it will stay in it's last
|
|
#define WP_YAW_BEHAVIOR_LOOK_AHEAD 3 // auto pilot will look ahead during missions and rtl (primarily meant for traditional helicotpers)
|
|
|
|
// TOY mixing options
|
|
#define TOY_LOOKUP_TABLE 0
|
|
#define TOY_LINEAR_MIXER 1
|
|
#define TOY_EXTERNAL_MIXER 2
|
|
|
|
|
|
// Waypoint options
|
|
#define MASK_OPTIONS_RELATIVE_ALT 1
|
|
#define WP_OPTION_ALT_CHANGE 2
|
|
#define WP_OPTION_YAW 4
|
|
#define WP_OPTION_ALT_REQUIRED 8
|
|
#define WP_OPTION_RELATIVE 16
|
|
//#define WP_OPTION_ 32
|
|
//#define WP_OPTION_ 64
|
|
#define WP_OPTION_NEXT_CMD 128
|
|
|
|
// RTL state
|
|
#define RTL_STATE_START 0
|
|
#define RTL_STATE_INITIAL_CLIMB 1
|
|
#define RTL_STATE_RETURNING_HOME 2
|
|
#define RTL_STATE_LOITERING_AT_HOME 3
|
|
#define RTL_STATE_FINAL_DESCENT 4
|
|
#define RTL_STATE_LAND 5
|
|
|
|
// LAND state
|
|
#define LAND_STATE_FLY_TO_LOCATION 0
|
|
#define LAND_STATE_DESCENDING 1
|
|
|
|
//repeating events
|
|
#define RELAY_TOGGLE 5
|
|
|
|
// GCS Message ID's
|
|
/// NOTE: to ensure we never block on sending MAVLink messages
|
|
/// please keep each MSG_ to a single MAVLink message. If need be
|
|
/// create new MSG_ IDs for additional messages on the same
|
|
/// stream
|
|
enum ap_message {
|
|
MSG_HEARTBEAT,
|
|
MSG_ATTITUDE,
|
|
MSG_LOCATION,
|
|
MSG_EXTENDED_STATUS1,
|
|
MSG_EXTENDED_STATUS2,
|
|
MSG_NAV_CONTROLLER_OUTPUT,
|
|
MSG_CURRENT_WAYPOINT,
|
|
MSG_VFR_HUD,
|
|
MSG_RADIO_OUT,
|
|
MSG_RADIO_IN,
|
|
MSG_RAW_IMU1,
|
|
MSG_RAW_IMU2,
|
|
MSG_RAW_IMU3,
|
|
MSG_GPS_RAW,
|
|
MSG_SERVO_OUT,
|
|
MSG_NEXT_WAYPOINT,
|
|
MSG_NEXT_PARAM,
|
|
MSG_STATUSTEXT,
|
|
MSG_LIMITS_STATUS,
|
|
MSG_AHRS,
|
|
MSG_SIMSTATE,
|
|
MSG_HWSTATUS,
|
|
MSG_RETRY_DEFERRED // this must be last
|
|
};
|
|
|
|
// Logging parameters
|
|
#define TYPE_AIRSTART_MSG 0x00
|
|
#define TYPE_GROUNDSTART_MSG 0x01
|
|
#define LOG_ATTITUDE_MSG 0x01
|
|
#define LOG_MODE_MSG 0x03
|
|
#define LOG_CONTROL_TUNING_MSG 0x04
|
|
#define LOG_NAV_TUNING_MSG 0x05
|
|
#define LOG_PERFORMANCE_MSG 0x06
|
|
#define LOG_CMD_MSG 0x08
|
|
#define LOG_CURRENT_MSG 0x09
|
|
#define LOG_STARTUP_MSG 0x0A
|
|
#define LOG_MOTORS_MSG 0x0B
|
|
#define LOG_OPTFLOW_MSG 0x0C
|
|
#define LOG_EVENT_MSG 0x0D
|
|
#define LOG_PID_MSG 0x0E
|
|
#define LOG_COMPASS_MSG 0x0F
|
|
#define LOG_DMP_MSG 0x10
|
|
#define LOG_INAV_MSG 0x11
|
|
#define LOG_CAMERA_MSG 0x12
|
|
#define LOG_ERROR_MSG 0x13
|
|
#define LOG_DATA_INT16_MSG 0x14
|
|
#define LOG_DATA_UINT16_MSG 0x15
|
|
#define LOG_DATA_INT32_MSG 0x16
|
|
#define LOG_DATA_UINT32_MSG 0x17
|
|
#define LOG_DATA_FLOAT_MSG 0x18
|
|
#define LOG_INDEX_MSG 0xF0
|
|
#define MAX_NUM_LOGS 50
|
|
|
|
#define MASK_LOG_ATTITUDE_FAST (1<<0)
|
|
#define MASK_LOG_ATTITUDE_MED (1<<1)
|
|
#define MASK_LOG_GPS (1<<2)
|
|
#define MASK_LOG_PM (1<<3)
|
|
#define MASK_LOG_CTUN (1<<4)
|
|
#define MASK_LOG_NTUN (1<<5)
|
|
#define MASK_LOG_MODE (1<<6) // not used
|
|
#define MASK_LOG_IMU (1<<7)
|
|
#define MASK_LOG_CMD (1<<8)
|
|
#define MASK_LOG_CURRENT (1<<9)
|
|
#define MASK_LOG_MOTORS (1<<10)
|
|
#define MASK_LOG_OPTFLOW (1<<11)
|
|
#define MASK_LOG_PID (1<<12)
|
|
#define MASK_LOG_COMPASS (1<<13)
|
|
#define MASK_LOG_INAV (1<<14)
|
|
#define MASK_LOG_CAMERA (1<<15)
|
|
|
|
// DATA - event logging
|
|
#define DATA_MAVLINK_FLOAT 1
|
|
#define DATA_MAVLINK_INT32 2
|
|
#define DATA_MAVLINK_INT16 3
|
|
#define DATA_MAVLINK_INT8 4
|
|
#define DATA_AP_STATE 7
|
|
#define DATA_INIT_SIMPLE_BEARING 9
|
|
#define DATA_ARMED 10
|
|
#define DATA_DISARMED 11
|
|
#define DATA_AUTO_ARMED 15
|
|
#define DATA_TAKEOFF 16
|
|
#define DATA_LAND_COMPLETE 18
|
|
#define DATA_LOST_GPS 19
|
|
#define DATA_BEGIN_FLIP 21
|
|
#define DATA_END_FLIP 22
|
|
#define DATA_EXIT_FLIP 23
|
|
#define DATA_SET_HOME 25
|
|
#define DATA_SET_SIMPLE_ON 26
|
|
#define DATA_SET_SIMPLE_OFF 27
|
|
|
|
// battery monitoring macros
|
|
#define BATTERY_VOLTAGE(x) (x->voltage_average()*g.volt_div_ratio)
|
|
#define CURRENT_AMPS(x) (x->voltage_average()-CURR_AMPS_OFFSET)*g.curr_amp_per_volt
|
|
|
|
#define BATT_MONITOR_DISABLED 0
|
|
#define BATT_MONITOR_VOLTAGE_ONLY 3
|
|
#define BATT_MONITOR_VOLTAGE_AND_CURRENT 4
|
|
|
|
/* ************************************************************** */
|
|
/* Expansion PIN's that people can use for various things. */
|
|
|
|
// AN0 - 7 are located at edge of IMU PCB "above" pressure sensor and
|
|
// Expansion port
|
|
// AN0 - 5 are also located next to voltage dividers and sliding SW2 switch
|
|
// AN0 - 3 has 10kOhm resistor in serial, include 3.9kOhm to make it as
|
|
// voltage divider
|
|
// AN4 - 5 are direct GPIO pins from atmega1280 and they are the latest pins
|
|
// next to SW2 switch
|
|
// Look more ArduCopter Wiki for voltage dividers and other ports
|
|
#define AN0 54 // resistor, vdiv use, divider 1 closest to relay
|
|
#define AN1 55 // resistor, vdiv use, divider 2
|
|
#define AN2 56 // resistor, vdiv use, divider 3
|
|
#define AN3 57 // resistor, vdiv use, divider 4 closest to SW2
|
|
#define AN4 58 // direct GPIO pin, default as analog input, next to SW2
|
|
// switch
|
|
#define AN5 59 // direct GPIO pin, default as analog input, next to SW2
|
|
// switch
|
|
#define AN6 60 // direct GPIO pin, default as analog input, close to
|
|
// Pressure sensor, Expansion Ports
|
|
#define AN7 61 // direct GPIO pin, default as analog input, close to
|
|
// Pressure sensor, Expansion Ports
|
|
|
|
// AN8 - 15 are located at edge of IMU PCB "above" pressure sensor and
|
|
// Expansion port
|
|
// AN8 - 15 PINs are not connected anywhere, they are located as last 8 pins
|
|
// on edge of the board above Expansion Ports
|
|
// even pins (8,10,12,14) are at edge of board, Odd pins (9,11,13,15) are on
|
|
// inner row
|
|
#define AN8 62 // NC
|
|
#define AN9 63 // NC
|
|
#define AN10 64 // NC
|
|
#define AN11 65 // NC
|
|
#define AN12 66 // NC
|
|
#define AN13 67 // NC
|
|
#define AN14 68 // NC
|
|
#define AN15 69 // NC
|
|
|
|
#define RELAY_APM1_PIN 47
|
|
#define RELAY_APM2_PIN 13
|
|
|
|
#define PIEZO_PIN AN5 //Last pin on the back ADC connector
|
|
|
|
// RADIANS
|
|
#define RADX100 0.000174532925f
|
|
#define DEGX100 5729.57795f
|
|
|
|
|
|
// EEPROM addresses
|
|
#define EEPROM_MAX_ADDR 4096
|
|
// parameters get the first 1536 bytes of EEPROM, remainder is for waypoints
|
|
#define WP_START_BYTE 0x600 // where in memory home WP is stored + all other
|
|
// WP
|
|
#define WP_SIZE 15
|
|
|
|
// fence points are stored at the end of the EEPROM
|
|
#define MAX_FENCEPOINTS 6
|
|
#define FENCE_WP_SIZE sizeof(Vector2l)
|
|
#define FENCE_START_BYTE (EEPROM_MAX_ADDR-(MAX_FENCEPOINTS*FENCE_WP_SIZE))
|
|
|
|
#define MAX_WAYPOINTS ((FENCE_START_BYTE - WP_START_BYTE) / WP_SIZE) - 1 // -
|
|
// 1
|
|
// to
|
|
// be
|
|
// safe
|
|
|
|
// mark a function as not to be inlined
|
|
#define NOINLINE __attribute__((noinline))
|
|
|
|
// IMU selection
|
|
#define CONFIG_IMU_OILPAN 1
|
|
#define CONFIG_IMU_MPU6000 2
|
|
#define CONFIG_IMU_SITL 3
|
|
#define CONFIG_IMU_PX4 4
|
|
|
|
#define AP_BARO_BMP085 1
|
|
#define AP_BARO_MS5611 2
|
|
#define AP_BARO_PX4 3
|
|
|
|
#define AP_BARO_MS5611_SPI 1
|
|
#define AP_BARO_MS5611_I2C 2
|
|
|
|
// Error message sub systems and error codes
|
|
#define ERROR_SUBSYSTEM_MAIN 1
|
|
#define ERROR_SUBSYSTEM_RADIO 2
|
|
#define ERROR_SUBSYSTEM_COMPASS 3
|
|
#define ERROR_SUBSYSTEM_OPTFLOW 4
|
|
#define ERROR_SUBSYSTEM_FAILSAFE_RADIO 5
|
|
#define ERROR_SUBSYSTEM_FAILSAFE_BATT 6
|
|
#define ERROR_SUBSYSTEM_FAILSAFE_GPS 7
|
|
#define ERROR_SUBSYSTEM_FAILSAFE_GCS 8
|
|
#define ERROR_SUBSYSTEM_FAILSAFE_FENCE 9
|
|
// general error codes
|
|
#define ERROR_CODE_ERROR_RESOLVED 0
|
|
#define ERROR_CODE_FAILED_TO_INITIALISE 1
|
|
// subsystem specific error codes -- radio
|
|
#define ERROR_CODE_RADIO_LATE_FRAME 2
|
|
// subsystem specific error codes -- failsafe_thr, batt, gps
|
|
#define ERROR_CODE_FAILSAFE_RESOLVED 0
|
|
#define ERROR_CODE_FAILSAFE_OCCURRED 1
|
|
// subsystem specific error codes -- compass
|
|
#define ERROR_CODE_COMPASS_FAILED_TO_READ 2
|
|
|
|
|
|
|
|
#endif // _DEFINES_H
|