mirror of https://github.com/ArduPilot/ardupilot
347 lines
9.8 KiB
C
347 lines
9.8 KiB
C
|
// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: t -*-
|
||
|
|
||
|
// Internal defines, don't edit and expect things to work
|
||
|
// -------------------------------------------------------
|
||
|
|
||
|
#define DEBUG 0
|
||
|
#define LOITER_RANGE 30 // for calculating power outside of loiter radius
|
||
|
|
||
|
// GPS baud rates
|
||
|
// --------------
|
||
|
#define NO_GPS 38400
|
||
|
#define NMEA_GPS 38400
|
||
|
#define EM406_GPS 57600
|
||
|
#define UBLOX_GPS 38400
|
||
|
#define ARDU_IMU 38400
|
||
|
#define MTK_GPS 38400
|
||
|
#define SIM_GPS 38400
|
||
|
|
||
|
// 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
|
||
|
|
||
|
// Radio channels
|
||
|
// Note channels are from 0!
|
||
|
//
|
||
|
// XXX these should be CH_n defines from RC.h at some point.
|
||
|
#define CH_ROLL 0
|
||
|
#define CH_PITCH 1
|
||
|
#define CH_THROTTLE 2
|
||
|
#define CH_RUDDER 3
|
||
|
#define CH_1 0
|
||
|
#define CH_2 1
|
||
|
#define CH_3 2
|
||
|
#define CH_4 3
|
||
|
#define CH_5 4
|
||
|
#define CH_6 5
|
||
|
#define CH_7 6
|
||
|
#define CH_8 7
|
||
|
|
||
|
#define WP_START_BYTE 0x130 // where in memory home WP is stored + all other WP
|
||
|
#define WP_SIZE 14
|
||
|
|
||
|
// GCS enumeration
|
||
|
#define GCS_PROTOCOL_STANDARD 0 // standard APM protocol
|
||
|
#define GCS_PROTOCOL_SPECIAL 1 // special test protocol (?)
|
||
|
#define GCS_PROTOCOL_LEGACY 2 // legacy ArduPilot protocol
|
||
|
#define GCS_PROTOCOL_XPLANE 3 // X-Plane HIL simulation
|
||
|
#define GCS_PROTOCOL_IMU 4 // ArdiPilot IMU output
|
||
|
#define GCS_PROTOCOL_JASON 5 // Jason's special secret GCS protocol
|
||
|
#define GCS_PROTOCOL_DEBUGTERMINAL 6 // Text-based interactive GCS
|
||
|
#define GCS_PROTOCOL_NONE -1 // No GCS output
|
||
|
|
||
|
// PID enumeration
|
||
|
// ---------------
|
||
|
#define CASE_SERVO_ROLL 0
|
||
|
#define CASE_SERVO_PITCH 1
|
||
|
#define CASE_SERVO_RUDDER 2
|
||
|
#define CASE_NAV_ROLL 3
|
||
|
#define CASE_NAV_PITCH_ASP 4
|
||
|
#define CASE_NAV_PITCH_ALT 5
|
||
|
#define CASE_TE_THROTTLE 6
|
||
|
#define CASE_ALT_THROTTLE 7
|
||
|
|
||
|
// Feedforward cases
|
||
|
// ----------------
|
||
|
#define CASE_PITCH_COMP 0
|
||
|
#define CASE_RUDDER_MIX 1
|
||
|
#define CASE_P_TO_T 2
|
||
|
#define CASE_T_TO_P 3
|
||
|
|
||
|
// Auto Pilot modes
|
||
|
// ----------------
|
||
|
#define MANUAL 0
|
||
|
#define CIRCLE 1 // When flying sans GPS, and we loose the radio, just circle
|
||
|
#define STABILIZE 2
|
||
|
|
||
|
#define FLY_BY_WIRE_A 5 // Fly By Wire A has left stick horizontal => desired roll angle, left stick vertical => desired pitch angle, right stick vertical = manual throttle
|
||
|
#define FLY_BY_WIRE_B 6 // Fly By Wire B has left stick horizontal => desired roll angle, left stick vertical => desired pitch angle, right stick vertical => desired airspeed
|
||
|
// Fly By Wire B = Fly By Wire A if you have AIRSPEED_SENSOR 0
|
||
|
#define AUTO 10
|
||
|
#define RTL 11
|
||
|
#define LOITER 12
|
||
|
#define TAKEOFF 13
|
||
|
#define LAND 14
|
||
|
|
||
|
|
||
|
// Command IDs - Must
|
||
|
#define CMD_BLANK 0x00 // there is no command stored in the mem location requested
|
||
|
#define CMD_WAYPOINT 0x10
|
||
|
#define CMD_LOITER 0x11
|
||
|
#define CMD_LOITER_N_TURNS 0x12
|
||
|
#define CMD_LOITER_TIME 0x13
|
||
|
#define CMD_RTL 0x14
|
||
|
#define CMD_LAND 0x15
|
||
|
#define CMD_TAKEOFF 0x16
|
||
|
|
||
|
// Command IDs - May
|
||
|
#define CMD_DELAY 0x20
|
||
|
#define CMD_CLIMB 0x21 // NOT IMPLEMENTED
|
||
|
#define CMD_LAND_OPTIONS 0x22 // pitch in deg, airspeed m/s, throttle %, track WP 1 or 0
|
||
|
|
||
|
// Command IDs - Now
|
||
|
//#define CMD_AP_MODE 0x30
|
||
|
#define CMD_RESET_INDEX 0x31
|
||
|
#define CMD_GOTO_INDEX 0x32 // NOT IMPLEMENTED
|
||
|
#define CMD_GETVAR_INDEX 0x33
|
||
|
#define CMD_SENDVAR_INDEX 0x34
|
||
|
#define CMD_TELEMETRY 0x35
|
||
|
|
||
|
#define CMD_THROTTLE_CRUISE 0x40
|
||
|
#define CMD_AIRSPEED_CRUISE 0x41
|
||
|
#define CMD_RESET_HOME 0x44
|
||
|
|
||
|
#define CMD_KP_GAIN 0x60
|
||
|
#define CMD_KI_GAIN 0x61
|
||
|
#define CMD_KD_GAIN 0x62
|
||
|
#define CMD_KI_MAX 0x63
|
||
|
#define CMD_KFF_GAIN 0x64
|
||
|
|
||
|
#define CMD_RADIO_TRIM 0x70
|
||
|
#define CMD_RADIO_MAX 0x71
|
||
|
#define CMD_RADIO_MIN 0x72
|
||
|
#define CMD_RADIO_MIN 0x72
|
||
|
#define CMD_ELEVON_TRIM 0x73
|
||
|
|
||
|
#define CMD_INDEX 0x75 // sets the current Must index
|
||
|
#define CMD_REPEAT 0x80
|
||
|
#define CMD_RELAY 0x81
|
||
|
#define CMD_SERVO 0x82 // move servo N to PWM value
|
||
|
|
||
|
//repeating events
|
||
|
#define NO_REPEAT 0
|
||
|
#define CH_4_TOGGLE 1
|
||
|
#define CH_5_TOGGLE 2
|
||
|
#define CH_6_TOGGLE 3
|
||
|
#define CH_7_TOGGLE 4
|
||
|
#define RELAY_TOGGLE 5
|
||
|
#define STOP_REPEAT 10
|
||
|
|
||
|
// GCS Message ID's
|
||
|
#define MSG_ACKNOWLEDGE 0x00
|
||
|
#define MSG_HEARTBEAT 0x01
|
||
|
#define MSG_ATTITUDE 0x02
|
||
|
#define MSG_LOCATION 0x03
|
||
|
#define MSG_PRESSURE 0x04
|
||
|
#define MSG_STATUS_TEXT 0x05
|
||
|
#define MSG_PERF_REPORT 0x06
|
||
|
#define MSG_COMMAND 0x22
|
||
|
#define MSG_VALUE 0x32
|
||
|
#define MSG_PID 0x42
|
||
|
#define MSG_TRIMS 0x50
|
||
|
#define MSG_MINS 0x51
|
||
|
#define MSG_MAXS 0x52
|
||
|
#define MSG_IMU_OUT 0x53
|
||
|
|
||
|
#define SEVERITY_LOW 1
|
||
|
#define SEVERITY_MEDIUM 2
|
||
|
#define SEVERITY_HIGH 3
|
||
|
#define SEVERITY_CRITICAL 4
|
||
|
|
||
|
// Logging parameters
|
||
|
#define LOG_ATTITUDE_MSG 0x01
|
||
|
#define LOG_GPS_MSG 0x02
|
||
|
#define LOG_MODE_MSG 0X03
|
||
|
#define LOG_CONTROL_TUNING_MSG 0X04
|
||
|
#define LOG_NAV_TUNING_MSG 0X05
|
||
|
#define LOG_PERFORMANCE_MSG 0X06
|
||
|
#define LOG_RAW_MSG 0x07
|
||
|
#define LOG_CMD_MSG 0x08
|
||
|
#define LOG_STARTUP_MSG 0x09
|
||
|
#define TYPE_AIRSTART_MSG 0x00
|
||
|
#define TYPE_GROUNDSTART_MSG 0x01
|
||
|
|
||
|
#define MASK_LOG_ATTITUDE_FAST 0
|
||
|
#define MASK_LOG_ATTITUDE_MED 2
|
||
|
#define MASK_LOG_GPS 4
|
||
|
#define MASK_LOG_PM 8
|
||
|
#define MASK_LOG_CTUN 16
|
||
|
#define MASK_LOG_NTUN 32
|
||
|
#define MASK_LOG_MODE 64
|
||
|
#define MASK_LOG_RAW 128
|
||
|
#define MASK_LOG_CMD 256
|
||
|
|
||
|
// Yaw modes
|
||
|
#define YAW_MODE_COORDINATE_TURNS 0
|
||
|
#define YAW_MODE_HOLD_HEADING 1
|
||
|
#define YAW_MODE_SLIP 2
|
||
|
|
||
|
// Waypoint Modes
|
||
|
// ----------------
|
||
|
#define ABS_WP 0
|
||
|
#define REL_WP 1
|
||
|
|
||
|
// Command Queues
|
||
|
// ---------------
|
||
|
#define COMMAND_MUST 0
|
||
|
#define COMMAND_MAY 1
|
||
|
#define COMMAND_NOW 2
|
||
|
|
||
|
// Events
|
||
|
// ------
|
||
|
#define EVENT_WILL_REACH_WAYPOINT 1
|
||
|
#define EVENT_SET_NEW_WAYPOINT_INDEX 2
|
||
|
#define EVENT_LOADED_WAYPOINT 3
|
||
|
#define EVENT_LOOP 4
|
||
|
|
||
|
//GPS_fix
|
||
|
#define VALID_GPS 0x00
|
||
|
#define BAD_GPS 0x01
|
||
|
#define FAILED_GPS 0x03
|
||
|
|
||
|
|
||
|
|
||
|
#define BATTERY_VOLTAGE(x) (x*(INPUT_VOLTAGE/1024.0))*VOLT_DIV_RATIO
|
||
|
|
||
|
#define AIRSPEED_CH 7 // The external ADC channel for the airspeed sensor
|
||
|
#define BATTERY_PIN1 0 // These are the pins for the voltage dividers
|
||
|
#define BATTERY_PIN2 1
|
||
|
#define BATTERY_PIN3 2
|
||
|
#define BATTERY_PIN4 3
|
||
|
#define RELAY_PIN 47
|
||
|
|
||
|
// Hardware Parameters
|
||
|
#define SLIDE_SWITCH_PIN 40
|
||
|
#define PUSHBUTTON_PIN 41
|
||
|
|
||
|
#define A_LED_PIN 37 //36 = B, 37 = A, 35 = C
|
||
|
#define B_LED_PIN 36
|
||
|
#define C_LED_PIN 35
|
||
|
|
||
|
#define HOLD_ALT_ABOVE_HOME 8 // bitmask value
|
||
|
|
||
|
// IMU Parameters
|
||
|
|
||
|
#define ADC_CONSTRAINT 900
|
||
|
#define TRUE 1
|
||
|
#define FALSE 0
|
||
|
#define ADC_WARM_CYCLES 200
|
||
|
#define SPEEDFILT 400 // centimeters/second
|
||
|
|
||
|
#define GYRO_TEMP_CH 3 // The ADC channel reading the gyro temperature
|
||
|
|
||
|
// ADC : Voltage reference 3.3v / 12bits(4096 steps) => 0.8mV/ADC step
|
||
|
// ADXL335 Sensitivity(from datasheet) => 330mV/g, 0.8mV/ADC step => 330/0.8 = 412
|
||
|
// Tested value : 418
|
||
|
#define GRAVITY 418 //this equivalent to 1G in the raw data coming from the accelerometer
|
||
|
#define Accel_Scale(x) x*(GRAVITY/9.81)//Scaling the raw data of the accel to actual acceleration in meters for seconds square
|
||
|
|
||
|
#define ToRad(x) (x*0.01745329252) // *pi/180
|
||
|
#define ToDeg(x) (x*57.2957795131) // *180/pi
|
||
|
|
||
|
// IDG500 Sensitivity (from datasheet) => 2.0mV/º/s, 0.8mV/ADC step => 0.8/3.33 = 0.4
|
||
|
// Tested values : 0.4026, ?, 0.4192
|
||
|
#define Gyro_Gain_X 0.4 //X axis Gyro gain
|
||
|
#define Gyro_Gain_Y 0.41 //Y axis Gyro gain
|
||
|
#define Gyro_Gain_Z 0.41 //Z axis Gyro gain
|
||
|
#define Gyro_Scaled_X(x) x*ToRad(Gyro_Gain_X) //Return the scaled ADC raw data of the gyro in radians for second
|
||
|
#define Gyro_Scaled_Y(x) x*ToRad(Gyro_Gain_Y) //Return the scaled ADC raw data of the gyro in radians for second
|
||
|
#define Gyro_Scaled_Z(x) x*ToRad(Gyro_Gain_Z) //Return the scaled ADC raw data of the gyro in radians for second
|
||
|
|
||
|
#define Kp_ROLLPITCH 0.0014 // Pitch&Roll Drift Correction Proportional Gain
|
||
|
#define Ki_ROLLPITCH 0.0000003 // Pitch&Roll Drift Correction Integrator Gain
|
||
|
#define Kp_YAW 0.8 // Yaw Drift Correction Porportional Gain
|
||
|
#define Ki_YAW 0.00004 // Yaw Drift CorrectionIntegrator Gain
|
||
|
|
||
|
/*For debugging purposes*/
|
||
|
#define OUTPUTMODE 1 //If value = 1 will print the corrected data, 0 will print uncorrected data of the gyros (with drift), 2 Accel only data
|
||
|
|
||
|
|
||
|
#define EEPROM_MAX_ADDR 4096
|
||
|
|
||
|
// Radio setup
|
||
|
#define EE_TRIM 0x00
|
||
|
#define EE_MIN 0x10
|
||
|
#define EE_MAX 0x20
|
||
|
#define EE_ELEVON1_TRIM 0x30
|
||
|
#define EE_ELEVON2_TRIM 0x32
|
||
|
|
||
|
// user gains
|
||
|
#define EE_XTRACK_GAIN 0x34
|
||
|
#define EE_XTRACK_ANGLE 0x36
|
||
|
#define EE_ALT_MIX 0x3B
|
||
|
#define EE_HEAD_MAX 0x38
|
||
|
#define EE_PITCH_MAX 0x39
|
||
|
#define EE_PITCH_MIN 0x3A
|
||
|
#define EE_KP 0x40
|
||
|
#define EE_KI 0x60
|
||
|
#define EE_KD 0x80
|
||
|
#define EE_IMAX 0xA0
|
||
|
#define EE_KFF 0xC0
|
||
|
#define EE_AN_OFFSET 0xE0
|
||
|
#define EE_PITCH_TARGET 0x127
|
||
|
|
||
|
//mission specific
|
||
|
#define EE_CONFIG 0X0F8
|
||
|
#define EE_WP_MODE 0x0F9
|
||
|
#define EE_YAW_MODE 0x0FA // not used
|
||
|
#define EE_WP_TOTAL 0x0FB
|
||
|
#define EE_WP_INDEX 0x0FC
|
||
|
#define EE_WP_RADIUS 0x0FD
|
||
|
#define EE_LOITER_RADIUS 0x0FE
|
||
|
#define EE_ALT_HOLD_HOME 0x0FF
|
||
|
|
||
|
// user configs
|
||
|
#define EE_AIRSPEED_CRUISE 0x103
|
||
|
#define EE_AIRSPEED_RATIO 0x104
|
||
|
#define EE_AIRSPEED_FBW_MIN 0x108
|
||
|
#define EE_AIRSPEED_FBW_MAX 0x109
|
||
|
#define EE_THROTTLE_MIN 0x10A
|
||
|
#define EE_THROTTLE_CRUISE 0x10B
|
||
|
#define EE_THROTTLE_MAX 0x10C
|
||
|
#define EE_THROTTLE_FAILSAFE 0x10D
|
||
|
#define EE_THROTTLE_FS_VALUE 0x10E
|
||
|
#define EE_THROTTLE_FAILSAFE_ACTION 0x110
|
||
|
#define EE_FLIGHT_MODE_CHANNEL 0x112
|
||
|
#define EE_AUTO_TRIM 0x113
|
||
|
#define EE_LOG_BITMASK 0x114
|
||
|
#define EE_REVERSE_SWITCH 0x120
|
||
|
#define EE_FLIGHT_MODES 0x121
|
||
|
|
||
|
// sensors
|
||
|
#define EE_ABS_PRESS_GND 0x116
|
||
|
#define EE_GND_TEMP 0x11A
|
||
|
#define EE_GND_ALT 0x11C
|
||
|
#define EE_AP_OFFSET 0x11E
|
||
|
|
||
|
// log
|
||
|
#define EE_LAST_LOG_PAGE 0xE00
|
||
|
#define EE_LAST_LOG_NUM 0xE02
|
||
|
#define EE_LOG_1_START 0xE04
|
||
|
|
||
|
// bits in log_bitmask
|
||
|
#define LOGBIT_ATTITUDE_FAST (1<<0)
|
||
|
#define LOGBIT_ATTITUDE_MED (1<<1)
|
||
|
#define LOGBIT_GPS (1<<2)
|
||
|
#define LOGBIT_PM (1<<3)
|
||
|
#define LOGBIT_CTUN (1<<4)
|
||
|
#define LOGBIT_NTUN (1<<5)
|
||
|
#define LOGBIT_MODE (1<<6)
|
||
|
#define LOGBIT_RAW (1<<7)
|
||
|
#define LOGBIT_CMD (1<<8)
|
||
|
|