ardupilot/Tools/VARTest/defines.h

// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-

#ifndef _DEFINES_H
#define _DEFINES_H

// 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 SERVO_MAX 4500	// This value represents 45 degrees and is just an arbitrary representation of servo max travel.

// failsafe
// ----------------------
#define FAILSAFE_NONE	0
#define FAILSAFE_SHORT	1
#define FAILSAFE_LONG	2
#define FAILSAFE_GCS	3
#define	FAILSAFE_SHORT_TIME 1500	// Miliiseconds
#define	FAILSAFE_LONG_TIME  20000	// Miliiseconds


// active altitude sensor
// ----------------------
#define SONAR 0
#define BARO 1

#define PITOT_SOURCE_ADC 1
#define PITOT_SOURCE_ANALOG_PIN 2

#define T6 1000000
#define T7 10000000

#define CH_ROLL CH_1
#define CH_PITCH CH_2
#define CH_THROTTLE CH_3
#define CH_RUDDER CH_4
#define CH_YAW CH_4

// HIL enumerations
#define HIL_MODE_DISABLED			0
#define HIL_MODE_SENSORS			1

// 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
#define FLY_BY_WIRE_C 7		// Fly By Wire C has left stick horizontal => desired roll angle, left stick vertical => desired climb rate, right stick vertical => desired airspeed
							// Fly By Wire B and Fly By Wire C require airspeed sensor
#define AUTO 10
#define RTL 11
#define LOITER 12
//#define TAKEOFF 13			// This is not used by APM.  It appears here for consistency with ACM
//#define LAND 14			// This is not used by APM.  It appears here for consistency with ACM
#define GUIDED 15
#define INITIALISING 16     // in startup routines


// 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
#define WAIT_COMMAND 255

// Command/Waypoint/Location Options Bitmask
//--------------------
#define MASK_OPTIONS_RELATIVE_ALT	(1<<0)		// 1 = Relative altitude

//repeating events
#define NO_REPEAT 0
#define CH_5_TOGGLE 1
#define CH_6_TOGGLE 2
#define CH_7_TOGGLE 3
#define CH_8_TOGGLE 4
#define RELAY_TOGGLE 5
#define STOP_REPEAT 10

#define MAV_CMD_CONDITION_YAW 23

//  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_STATUS,
    MSG_GPS_RAW,
    MSG_SERVO_OUT,
    MSG_NEXT_WAYPOINT,
    MSG_NEXT_PARAM,
    MSG_STATUSTEXT,
    MSG_FENCE_STATUS,
    MSG_RETRY_DEFERRED // this must be last
};

// 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_COMMAND_INDEX 2
#define EVENT_LOADED_WAYPOINT 3
#define EVENT_LOOP 4

// Climb rate calculations
#define	ALTITUDE_HISTORY_LENGTH 8	//Number of (time,altitude) points to regress a climb rate from


#define BATTERY_VOLTAGE(x) (x*(g.input_voltage/1024.0))*g.volt_div_ratio
#define CURRENT_AMPS(x) ((x*(g.input_voltage/1024.0))-CURR_AMPS_OFFSET)*g.curr_amp_per_volt

#define RELAY_PIN 47


// sonar
#define MAX_SONAR_XL 0
#define MAX_SONAR_LV 1
#define SonarToCm(x) (x*1.26)   // Sonar raw value to centimeters
#define AN4			4
#define AN5			5

#define SPEEDFILT 400			// centimeters/second; the speed below which a groundstart will be triggered


// EEPROM addresses
#define EEPROM_MAX_ADDR		4096
// parameters get the first 1KiB of EEPROM, remainder is for waypoints
#define WP_START_BYTE 0x400 // 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 20
#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

// convert a boolean (0 or 1) to a sign for multiplying (0 maps to 1, 1 maps to -1)
#define BOOL_TO_SIGN(bvalue) ((bvalue)?-1:1)

// mark a function as not to be inlined
#define NOINLINE __attribute__((noinline))

#define CONFIG_IMU_OILPAN 1
#define CONFIG_IMU_MPU6000 2

#define AP_BARO_BMP085   1
#define AP_BARO_MS5611   2

#endif // _DEFINES_H