2011-03-19 07:20:11 -03:00
// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
2010-12-19 12:40:33 -04:00
2011-10-11 06:12:37 -03:00
# ifndef _DEFINES_H
# define _DEFINES_H
2012-12-13 20:32:36 -04:00
# include <AP_HAL_Boards.h>
2011-06-01 02:50:17 -03:00
// Just so that it's completely clear...
2012-08-16 21:50:03 -03:00
# define ENABLED 1
# define DISABLED 0
2011-02-24 01:56:59 -04:00
2012-03-07 03:40:04 -04:00
// this avoids a very common config error
# define ENABLE ENABLED
# define DISABLE DISABLED
2011-09-04 21:15:36 -03:00
// Flight modes
// ------------
2012-12-08 01:23:32 -04:00
# 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)
2013-03-22 05:38:07 -03:00
# 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
2013-11-13 13:57:48 -04:00
# define YAW_DRIFT 8 //
2013-05-20 22:58:34 -03:00
# define YAW_RESETTOARMEDYAW 9 // point towards heading at time motors were armed
2011-09-04 21:15:36 -03:00
2013-02-18 01:58:24 -04:00
# define ROLL_PITCH_STABLE 0 // pilot input roll, pitch angles
2013-08-04 03:56:35 -03:00
# define ROLL_PITCH_ACRO 1 // pilot inputs roll, pitch rotation rates in body frame
2013-02-18 01:58:24 -04:00
# 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
2013-11-13 13:57:48 -04:00
# define ROLL_PITCH_DRIFT 4 //
2013-02-18 01:58:24 -04:00
# define ROLL_PITCH_LOITER 5 // pilot inputs the desired horizontal velocities
2013-08-04 03:56:35 -03:00
# define ROLL_PITCH_SPORT 6 // pilot inputs roll, pitch rotation rates in earth frame
2013-09-03 06:31:06 -03:00
# define ROLL_PITCH_AUTOTUNE 7 // description of new roll-pitch mode
2011-09-04 21:15:36 -03:00
2012-11-23 02:57:49 -04:00
# 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
2013-04-17 10:14:22 -03:00
# 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
2013-11-06 01:51:28 -04:00
# define THROTTLE_MANUAL_HELI 5 // pilot manually controlled throttle for traditional helicopters
2011-09-04 21:15:36 -03:00
2013-03-18 01:40:43 -03:00
// sonar - for use with CONFIG_SONAR_SOURCE
2011-11-12 23:37:16 -04:00
# define SONAR_SOURCE_ADC 1
# define SONAR_SOURCE_ANALOG_PIN 2
2013-07-27 20:28:00 -03:00
// Ch6, Ch7 and Ch8 aux switch control
2013-07-29 04:28:04 -03:00
# define AUX_SWITCH_PWM_TRIGGER_HIGH 1800 // pwm value above which the ch7 or ch8 option will be invoked
# define AUX_SWITCH_PWM_TRIGGER_LOW 1200 // pwm value below which the ch7 or ch8 option will be disabled
2013-05-17 02:42:28 -03:00
# 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
2013-07-20 03:00:08 -03:00
# define AUX_SWITCH_FENCE 11 // allow enabling or disabling fence in flight
2013-05-20 16:26:39 -03:00
# define AUX_SWITCH_RESETTOARMEDYAW 12 // changes yaw to be same as when quad was armed
2013-07-29 04:28:04 -03:00
# define AUX_SWITCH_SUPERSIMPLE_MODE 13 // change to simple mode in middle, super simple at top
2013-08-04 06:33:23 -03:00
# define AUX_SWITCH_ACRO_TRAINER 14 // low = disabled, middle = leveled, high = leveled and limited
2013-08-04 11:38:38 -03:00
# define AUX_SWITCH_SPRAYER 15 // enable/disable the crop sprayer
2013-08-19 06:09:23 -03:00
# define AUX_SWITCH_AUTO 16 // change to auto flight mode
2013-09-03 06:31:06 -03:00
# define AUX_SWITCH_AUTOTUNE 17 // auto tune
2013-10-22 01:13:36 -03:00
# define AUX_SWITCH_LAND 18 // change to LAND flight mode
2011-08-05 13:22:43 -03:00
2013-07-29 04:28:04 -03:00
// values used by the ap.ch7_opt and ap.ch8_opt flags
# define AUX_SWITCH_LOW 0 // indicates auxiliar switch is in the low position (pwm <1200)
# define AUX_SWITCH_MIDDLE 1 // indicates auxiliar switch is in the middle position (pwm >1200, <1800)
# define AUX_SWITCH_HIGH 2 // indicates auxiliar switch is in the high position (pwm >1800)
2012-12-19 12:08:59 -04:00
2011-02-24 01:56:59 -04:00
// Frame types
2013-09-09 03:57:54 -03:00
# define UNDEFINED_FRAME 0
# define QUAD_FRAME 1
# define TRI_FRAME 2
# define HEXA_FRAME 3
# define Y6_FRAME 4
# define OCTA_FRAME 5
# define HELI_FRAME 6
# define OCTA_QUAD_FRAME 7
2013-11-12 09:51:48 -04:00
# define SINGLE_FRAME 8
2011-05-18 20:38:24 -03:00
# define PLUS_FRAME 0
# define X_FRAME 1
2011-06-24 01:37:54 -03:00
# define V_FRAME 2
2011-06-16 14:03:26 -03:00
// LED output
# define NORMAL_LEDS 0
2012-11-05 00:32:38 -04:00
# define SAVE_TRIM_LEDS 1
2011-06-16 14:03:26 -03:00
2011-06-28 03:31:18 -03:00
2010-12-19 12:40:33 -04:00
// Internal defines, don't edit and expect things to work
// -------------------------------------------------------
2011-02-19 03:44:44 -04:00
# define TRUE 1
# define FALSE 0
2012-12-19 02:02:13 -04:00
# define ToRad(x) radians(x) // *pi/180
# define ToDeg(x) degrees(x) // *180/pi
2011-02-19 03:44:44 -04:00
2010-12-19 12:40:33 -04:00
# define DEBUG 0
2011-03-13 03:25:38 -03:00
# define LOITER_RANGE 60 // for calculating power outside of loiter radius
2010-12-19 12:40:33 -04:00
2011-02-17 03:09:13 -04:00
# define T6 1000000
# define T7 10000000
2010-12-19 12:40:33 -04:00
// GPS type codes - use the names, not the numbers
2012-08-16 21:50:03 -03:00
# 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
2012-12-21 15:19:32 -04:00
# define GPS_PROTOCOL_MTK19 6
2012-08-16 21:50:03 -03:00
# define GPS_PROTOCOL_AUTO 7
2010-12-19 12:40:33 -04:00
2011-02-19 03:44:44 -04:00
// HIL enumerations
2012-11-10 01:55:51 -04:00
# define HIL_MODE_DISABLED 0
# define HIL_MODE_ATTITUDE 1
# define HIL_MODE_SENSORS 2
2011-02-19 03:44:44 -04:00
2012-12-09 03:44:42 -04:00
// Altitude status definitions
2012-08-16 21:50:03 -03:00
# define REACHED_ALT 0
2012-11-10 01:55:51 -04:00
# define DESCENDING 1
# define ASCENDING 2
2012-01-10 19:44:26 -04:00
2010-12-19 12:40:33 -04:00
// Auto Pilot modes
// ----------------
2012-08-16 21:50:03 -03:00
# 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
2013-08-04 03:56:35 -03:00
# define OF_LOITER 10 // Hold a single location using optical flow sensor
2013-11-13 13:57:48 -04:00
# define DRIFT 11 // DRIFT mode (Note: 12 is no longer used)
2013-08-04 03:56:35 -03:00
# define SPORT 13 // earth frame rate control
# define NUM_MODES 14
2011-09-14 17:58:18 -03:00
2013-10-29 01:28:27 -03:00
2011-04-17 20:08:16 -03:00
// CH_6 Tuning
2011-04-18 13:27:03 -03:00
// -----------
2013-06-30 06:51:43 -03:00
# define CH6_NONE 0 // no tuning performed
# define CH6_STABILIZE_ROLL_PITCH_KP 1 // stabilize roll/pitch angle controller's P term
# define CH6_RATE_ROLL_PITCH_KP 4 // body frame roll/pitch rate controller's P term
# define CH6_RATE_ROLL_PITCH_KI 5 // body frame roll/pitch rate controller's I term
# define CH6_RATE_ROLL_PITCH_KD 21 // body frame roll/pitch rate controller's D term
# define CH6_STABILIZE_YAW_KP 3 // stabilize yaw heading controller's P 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_ALTITUDE_HOLD_KP 14 // altitude hold controller's P term (alt error to desired rate)
# define CH6_THROTTLE_RATE_KP 7 // throttle rate controller's P term (desired rate to acceleration or motor output)
# define CH6_THROTTLE_RATE_KD 37 // throttle rate controller's D term (desired rate to acceleration or motor output)
# define CH6_THROTTLE_ACCEL_KP 34 // accel based throttle controller's P term
# define CH6_THROTTLE_ACCEL_KI 35 // accel based throttle controller's I term
# define CH6_THROTTLE_ACCEL_KD 36 // accel based throttle controller's D term
# define CH6_LOITER_POSITION_KP 12 // loiter distance controller's P term (position error to speed)
# 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_WP_SPEED 10 // maximum speed to next way point (0 to 10m/s)
2013-08-04 08:22:12 -03:00
# define CH6_ACRO_RP_KP 25 // acro controller's P term. converts pilot input to a desired roll, pitch or yaw rate
# define CH6_ACRO_YAW_KP 40 // acro controller's P term. converts pilot input to a desired roll, pitch or yaw rate
2013-06-30 06:51:43 -03:00
# define CH6_RELAY 9 // switch relay on if ch6 high, off if low
# 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_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)
2013-08-18 03:44:54 -03:00
# define CH6_SONAR_GAIN 41 // sonar gain
2011-11-20 09:30:42 -04:00
2013-08-04 06:14:07 -03:00
// Acro Trainer types
# define ACRO_TRAINER_DISABLED 0
# define ACRO_TRAINER_LEVELING 1
# define ACRO_TRAINER_LIMITED 2
2011-03-05 00:56:58 -04:00
2012-08-16 21:50:03 -03:00
// 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
2011-03-02 22:32:50 -04:00
# define NO_COMMAND 0
2011-03-27 18:26:34 -03:00
2013-01-24 00:36:55 -04:00
// Navigation modes held in nav_mode variable
# define NAV_NONE 0
# define NAV_CIRCLE 1
# define NAV_LOITER 2
# define NAV_WP 3
2011-04-26 02:15:25 -03:00
2013-04-18 03:30:18 -03:00
// 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
2013-11-13 13:57:48 -04:00
# 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
2013-04-20 03:36:24 -03:00
# define WP_YAW_BEHAVIOR_LOOK_AHEAD 3 // auto pilot will look ahead during missions and rtl (primarily meant for traditional helicotpers)
2012-12-09 05:04:31 -04:00
2012-08-09 20:49:44 -03:00
2011-04-08 16:13:31 -03:00
// Waypoint options
2012-08-16 21:50:03 -03:00
# define MASK_OPTIONS_RELATIVE_ALT 1
# define WP_OPTION_ALT_CHANGE 2
2012-11-10 01:55:51 -04:00
# define WP_OPTION_YAW 4
2012-08-16 21:50:03 -03:00
# define WP_OPTION_ALT_REQUIRED 8
2012-11-10 01:55:51 -04:00
# define WP_OPTION_RELATIVE 16
2011-04-08 16:13:31 -03:00
//#define WP_OPTION_ 32
//#define WP_OPTION_ 64
2012-11-10 01:55:51 -04:00
# define WP_OPTION_NEXT_CMD 128
2011-04-08 16:13:31 -03:00
2012-11-29 08:08:19 -04:00
// RTL state
2013-04-08 23:58:01 -03:00
# 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
2012-11-29 08:08:19 -04:00
2013-05-10 10:37:15 -03:00
// LAND state
# define LAND_STATE_FLY_TO_LOCATION 0
# define LAND_STATE_DESCENDING 1
2010-12-19 12:40:33 -04:00
//repeating events
# define RELAY_TOGGLE 5
// GCS Message ID's
2011-10-11 06:12:37 -03:00
/// 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 ,
2013-10-23 08:15:21 -03:00
MSG_SYSTEM_TIME ,
2011-10-11 06:12:37 -03:00
MSG_SERVO_OUT ,
MSG_NEXT_WAYPOINT ,
MSG_NEXT_PARAM ,
MSG_STATUSTEXT ,
2012-07-14 23:26:17 -03:00
MSG_LIMITS_STATUS ,
2012-03-11 05:36:12 -03:00
MSG_AHRS ,
2012-03-01 08:36:35 -04:00
MSG_SIMSTATE ,
MSG_HWSTATUS ,
2011-10-11 06:12:37 -03:00
MSG_RETRY_DEFERRED // this must be last
} ;
2010-12-19 12:40:33 -04:00
// Logging parameters
2012-08-16 21:50:03 -03:00
# define TYPE_AIRSTART_MSG 0x00
2012-09-11 00:26:48 -03:00
# define TYPE_GROUNDSTART_MSG 0x01
2012-08-16 21:50:03 -03:00
# define LOG_ATTITUDE_MSG 0x01
2012-09-27 05:40:54 -03:00
# define LOG_MODE_MSG 0x03
# define LOG_CONTROL_TUNING_MSG 0x04
# define LOG_NAV_TUNING_MSG 0x05
# define LOG_PERFORMANCE_MSG 0x06
2012-09-11 00:26:48 -03:00
# define LOG_CMD_MSG 0x08
2012-08-16 21:50:03 -03:00
# define LOG_CURRENT_MSG 0x09
# define LOG_STARTUP_MSG 0x0A
# define LOG_MOTORS_MSG 0x0B
# define LOG_OPTFLOW_MSG 0x0C
2013-01-12 11:17:44 -04:00
# define LOG_EVENT_MSG 0x0D
2012-08-16 21:50:03 -03:00
# define LOG_PID_MSG 0x0E
2013-02-09 02:24:02 -04:00
# define LOG_COMPASS_MSG 0x0F
2012-11-07 06:03:30 -04:00
# define LOG_INAV_MSG 0x11
2012-12-06 11:57:08 -04:00
# define LOG_CAMERA_MSG 0x12
2012-12-29 23:08:25 -04:00
# define LOG_ERROR_MSG 0x13
2013-01-12 11:17:44 -04:00
# 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
2013-09-03 06:31:06 -03:00
# define LOG_AUTOTUNE_MSG 0x19
# define LOG_AUTOTUNEDETAILS_MSG 0x1A
2012-08-16 21:50:03 -03:00
# define LOG_INDEX_MSG 0xF0
# define MAX_NUM_LOGS 50
2012-11-10 01:55:51 -04:00
# define MASK_LOG_ATTITUDE_FAST (1<<0)
# define MASK_LOG_ATTITUDE_MED (1<<1)
2012-08-16 21:50:03 -03:00
# define MASK_LOG_GPS (1<<2)
# define MASK_LOG_PM (1<<3)
# define MASK_LOG_CTUN (1<<4)
# define MASK_LOG_NTUN (1<<5)
2013-05-17 00:26:42 -03:00
# define MASK_LOG_MODE (1<<6) // not used
2013-01-12 11:17:44 -04:00
# define MASK_LOG_IMU (1<<7)
2012-08-16 21:50:03 -03:00
# define MASK_LOG_CMD (1<<8)
2013-01-26 04:20:41 -04:00
# define MASK_LOG_CURRENT (1<<9)
2012-08-16 21:50:03 -03:00
# define MASK_LOG_MOTORS (1<<10)
# define MASK_LOG_OPTFLOW (1<<11)
# define MASK_LOG_PID (1<<12)
2013-02-09 02:24:02 -04:00
# define MASK_LOG_COMPASS (1<<13)
2012-11-07 06:03:30 -04:00
# define MASK_LOG_INAV (1<<14)
2012-12-06 11:57:08 -04:00
# define MASK_LOG_CAMERA (1<<15)
2012-11-10 01:55:51 -04:00
// 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
2013-07-26 02:15:27 -03:00
# define DATA_NOT_LANDED 28
2012-11-10 01:55:51 -04:00
# 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
2013-10-19 09:53:51 -03:00
# define DATA_SET_SUPERSIMPLE_ON 29
# define DATA_AUTOTUNE_INITIALISED 30
# define DATA_AUTOTUNE_OFF 31
# define DATA_AUTOTUNE_RESTART 32
# define DATA_AUTOTUNE_COMPLETE 33
# define DATA_AUTOTUNE_ABANDONED 34
# define DATA_AUTOTUNE_REACHED_LIMIT 35
# define DATA_AUTOTUNE_TESTING 36
# define DATA_AUTOTUNE_SAVEDGAINS 37
2013-10-31 23:53:16 -03:00
# define DATA_SAVE_TRIM 38
# define DATA_SAVEWP_ADD_WP 39
# define DATA_SAVEWP_CLEAR_MISSION_RTL 40
# define DATA_FENCE_ENABLE 41
# define DATA_FENCE_DISABLE 42
# define DATA_ACRO_TRAINER_DISABLED 43
# define DATA_ACRO_TRAINER_LEVELING 44
# define DATA_ACRO_TRAINER_LIMITED 45
2013-10-18 01:57:50 -03:00
2012-11-10 01:55:51 -04:00
2011-05-20 14:40:11 -03:00
/* ************************************************************** */
/* Expansion PIN's that people can use for various things. */
2012-08-16 21:50:03 -03:00
// AN0 - 7 are located at edge of IMU PCB "above" pressure sensor and
// Expansion port
2011-05-20 14:40:11 -03:00
// AN0 - 5 are also located next to voltage dividers and sliding SW2 switch
2012-08-16 21:50:03 -03:00
// 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
2011-05-20 14:40:11 -03:00
// 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
2012-08-16 21:50:03 -03:00
# 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
2011-05-20 14:40:11 -03:00
# 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
2012-12-22 04:26:27 -04:00
# define RELAY_APM1_PIN 47
# define RELAY_APM2_PIN 13
2010-12-19 12:40:33 -04:00
2011-06-03 02:36:39 -03:00
# define PIEZO_PIN AN5 //Last pin on the back ADC connector
2011-11-19 15:08:03 -04:00
// RADIANS
2013-01-10 14:42:24 -04:00
# define RADX100 0.000174532925f
# define DEGX100 5729.57795f
2011-12-03 19:28:36 -04:00
2010-12-19 12:40:33 -04:00
// EEPROM addresses
2012-08-16 21:50:03 -03:00
# define EEPROM_MAX_ADDR 4096
2012-05-30 21:41:53 -03:00
// parameters get the first 1536 bytes of EEPROM, remainder is for waypoints
2012-08-16 21:50:03 -03:00
# define WP_START_BYTE 0x600 // where in memory home WP is stored + all other
// WP
2011-03-26 03:35:52 -03:00
# define WP_SIZE 15
2011-05-09 14:40:32 -03:00
2012-07-14 23:26:17 -03:00
// fence points are stored at the end of the EEPROM
2012-10-22 04:57:08 -03:00
# define MAX_FENCEPOINTS 6
2012-07-14 23:26:17 -03:00
# define FENCE_WP_SIZE sizeof(Vector2l)
# define FENCE_START_BYTE (EEPROM_MAX_ADDR-(MAX_FENCEPOINTS*FENCE_WP_SIZE))
2012-08-16 21:50:03 -03:00
# define MAX_WAYPOINTS ((FENCE_START_BYTE - WP_START_BYTE) / WP_SIZE) - 1 // -
// 1
// to
// be
// safe
2011-10-11 06:12:37 -03:00
// mark a function as not to be inlined
# define NOINLINE __attribute__((noinline))
2011-11-12 23:37:16 -04:00
// IMU selection
2012-12-18 06:15:11 -04:00
# define CONFIG_IMU_OILPAN 1
2011-11-12 23:37:16 -04:00
# define CONFIG_IMU_MPU6000 2
2012-12-18 06:15:11 -04:00
# define CONFIG_IMU_SITL 3
2013-01-05 05:38:19 -04:00
# define CONFIG_IMU_PX4 4
2013-09-23 04:06:51 -03:00
# define CONFIG_IMU_FLYMAPLE 5
2011-11-12 23:37:16 -04:00
2011-11-27 02:07:00 -04:00
# define AP_BARO_BMP085 1
# define AP_BARO_MS5611 2
2013-01-05 05:38:19 -04:00
# define AP_BARO_PX4 3
2011-11-27 02:07:00 -04:00
2013-01-08 14:25:51 -04:00
# define AP_BARO_MS5611_SPI 1
# define AP_BARO_MS5611_I2C 2
2012-12-29 23:08:25 -04:00
// 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
2013-03-16 05:14:21 -03:00
# define ERROR_SUBSYSTEM_FAILSAFE_RADIO 5
# define ERROR_SUBSYSTEM_FAILSAFE_BATT 6
# define ERROR_SUBSYSTEM_FAILSAFE_GPS 7
2013-04-29 09:30:22 -03:00
# define ERROR_SUBSYSTEM_FAILSAFE_GCS 8
# define ERROR_SUBSYSTEM_FAILSAFE_FENCE 9
2013-09-24 08:47:54 -03:00
# define ERROR_SUBSYSTEM_FLIGHT_MODE 10
2013-09-23 00:20:57 -03:00
# define ERROR_SUBSYSTEM_GPS 11
2013-10-29 10:11:48 -03:00
# define ERROR_SUBSYSTEM_CRASH_CHECK 12
2012-12-29 23:08:25 -04:00
// 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
2013-03-16 05:14:21 -03:00
// subsystem specific error codes -- failsafe_thr, batt, gps
# define ERROR_CODE_FAILSAFE_RESOLVED 0
# define ERROR_CODE_FAILSAFE_OCCURRED 1
2013-05-13 06:01:30 -03:00
// subsystem specific error codes -- compass
# define ERROR_CODE_COMPASS_FAILED_TO_READ 2
2013-09-23 00:20:57 -03:00
// subsystem specific error codes -- gps
# define ERROR_CODE_GPS_GLITCH 2
2013-10-08 03:30:43 -03:00
// subsystem specific error codes -- main
2013-10-29 10:11:48 -03:00
# define ERROR_CODE_MAIN_INS_DELAY 1
// subsystem specific error codes -- crash checker
# define ERROR_CODE_CRASH_CHECK_CRASH 1
2012-12-29 23:08:25 -04:00
2013-11-15 04:12:31 -04:00
// Arming Check Enable/Disable bits
# define ARMING_CHECK_NONE 0x00
# define ARMING_CHECK_ALL 0x01
# define ARMING_CHECK_BARO 0x02
# define ARMING_CHECK_COMPASS 0x04
# define ARMING_CHECK_GPS 0x08
# define ARMING_CHECK_INS 0x10
# define ARMING_CHECK_PARAMETERS 0x20
# define ARMING_CHECK_RC 0x40
# define ARMING_CHECK_VOLTAGE 0x80
2012-12-29 23:08:25 -04:00
2013-11-16 00:55:59 -04:00
// Radio failsafe definitions (FS_THR parameter)
# define FS_THR_DISABLED 0
# define FS_THR_ENABLED_ALWAYS_RTL 1
# define FS_THR_ENABLED_CONTINUE_MISSION 2
# define FS_THR_ENABLED_ALWAYS_LAND 3
2013-11-16 01:46:57 -04:00
// Battery failsafe definitions (FS_BATT_ENABLE parameter)
# define FS_BATT_DISABLED 0 // battery failsafe disabled
# define FS_BATT_LAND 1 // switch to LAND mode on battery failsafe
# define FS_BATT_RTL 2 // switch to RTL mode on battery failsafe
2013-11-16 00:55:59 -04:00
// GPS Failsafe definitions (FS_GPS_ENABLE parameter)
# define FS_GPS_DISABLED 0 // GPS failsafe disabled
# define FS_GPS_LAND 1 // switch to LAND mode on GPS Failsafe
# define FS_GPS_ALTHOLD 2 // switch to ALTHOLD mode on GPS failsafe
# define FS_GPS_LAND_EVEN_STABILIZE 3 // switch to LAND mode on GPS failsafe even if in a manual flight mode like Stabilize
2011-10-11 06:12:37 -03:00
# endif // _DEFINES_H