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MultiWii.h
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MultiWii.h
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#ifndef MULTIWII_H_
#define MULTIWII_H_
#define VERSION 231
#define NAVI_VERSION 7 //This allow sync with GUI
#include "types.h"
#include "Alarms.h"
#define MINCHECK 1100
#define MAXCHECK 1900
extern volatile unsigned long timer0_overflow_count;
extern const char pidnames[];
extern const char boxnames[];
extern const uint8_t boxids[];
extern uint32_t currentTime;
extern uint16_t previousTime;
extern uint16_t cycleTime;
extern uint16_t calibratingA;
extern uint16_t calibratingB;
extern uint16_t calibratingG;
extern int16_t magHold,headFreeModeHold;
extern uint8_t vbatMin;
extern uint8_t rcOptions[CHECKBOXITEMS];
extern int32_t AltHold;
extern int16_t sonarAlt;
extern int16_t BaroPID;
extern int16_t errorAltitudeI;
extern int16_t i2c_errors_count;
extern uint8_t alarmArray[ALRM_FAC_SIZE];
extern global_conf_t global_conf;
extern imu_t imu;
extern analog_t analog;
extern alt_t alt;
extern att_t att;
#ifdef LOG_PERMANENT
extern plog_t plog;
#endif
extern int16_t debug[4];
extern conf_t conf;
extern int16_t annex650_overrun_count;
extern flags_struct_t f;
extern uint16_t intPowerTrigger1;
extern int16_t gyroZero[3];
extern int16_t angle[2];
#if BARO
extern int32_t baroPressure;
extern int16_t baroTemperature; // temp in 0.01 deg
extern int32_t baroPressureSum;
#endif
extern int16_t axisPID[3];
extern int16_t motor[8];
extern int16_t servo[8];
extern int16_t failsafeEvents;
extern volatile int16_t failsafeCnt;
extern int16_t rcData[RC_CHANS];
extern int16_t rcSerial[8];
extern int16_t rcCommand[4];
extern uint8_t rcSerialCount;
extern int16_t lookupPitchRollRC[5];
extern uint16_t lookupThrottleRC[11];
#if defined(POWERMETER) || ( defined(LOG_VALUES) && (LOG_VALUES >= 3) )
#define PMOTOR_SUM 8 // index into pMeter[] for sum
extern uint32_t pMeter[PMOTOR_SUM + 1]; // we use [0:7] for eight motors,one extra for sum
extern uint8_t pMeterV; // dummy to satisfy the paramStruct logic in ConfigurationLoop()
extern uint32_t pAlarm; // we scale the eeprom value from [0:255] to this value we can directly compare to the sum in pMeter[6]
extern uint16_t powerValue; // last known current
#endif
#if defined(LCD_TELEMETRY)
extern uint8_t telemetry;
extern uint8_t telemetry_auto;
#endif
#ifdef LCD_TELEMETRY_STEP
extern char telemetryStepSequence[];
extern uint8_t telemetryStepIndex;
#endif
#if defined(LOG_VALUES) || defined(LCD_TELEMETRY)
extern uint16_t cycleTimeMax; // highest ever cycle timen
extern uint16_t cycleTimeMin; // lowest ever cycle timen
extern int32_t BAROaltMax; // maximum value
extern uint16_t GPS_speedMax; // maximum speed from gps
extern uint16_t powerValueMaxMAH;
extern uint16_t wattsMax;
#endif
#if defined(LOG_VALUES) || defined(LCD_TELEMETRY) || defined(ARMEDTIMEWARNING) || defined(LOG_PERMANENT)
extern uint32_t armedTime;
#endif
#if GPS
// *************************************** begin GPS common variables and defines ******************************************************************
extern gps_conf_struct GPS_conf;
extern int16_t GPS_angle[2]; // the angles that must be applied for GPS correction
extern int32_t GPS_coord[2];
extern int32_t GPS_home[2];
extern int32_t GPS_hold[2];
extern int32_t GPS_prev[2];
extern int32_t GPS_poi[2]; // Coordinates of the current poi
extern int32_t GPS_directionToPoi; // direction to the actual poi (used to set heading to poi)
extern uint8_t GPS_numSat;
extern uint16_t GPS_distanceToHome; // distance to home - unit: meter
extern int16_t GPS_directionToHome; // direction to home - unit: degree
extern uint16_t GPS_altitude; // GPS altitude - unit: meter
extern uint16_t GPS_speed; // GPS speed - unit: cm/s
extern uint8_t GPS_update; // a binary toogle to distinct a GPS position update
extern uint16_t GPS_ground_course; // - unit: degree*10
extern uint32_t GPS_time;
extern uint8_t GPS_mode; // contains the current selected gps flight mode
extern uint8_t NAV_error; //Last error situation of the nav engine
extern uint8_t NAV_state; //State of the nav engine
extern uint8_t GPS_saved_mission_state; //The mission state saved when poshold invoked during mission
extern uint8_t prv_gps_modes; //GPS_checkbox items packed into 1 byte for checking GPS mode changes
extern uint32_t nav_timer_stop; //common timer used in navigation (contains the desired stop time in millis()
extern uint16_t nav_hold_time; //time in seconds to hold position
extern uint8_t NAV_paused_at; //This contains the mission step where poshold paused the runing mission.
extern uint8_t next_step; //The mission step which is upcoming it equals with the mission_step stored in EEPROM
//Altitude control state
#define ASCENDING 1
#define DESCENDING -1
#define REACHED_ALT 0
// The orginal altitude used as base our new altitude during nav
extern int32_t original_altitude;
//This is the target what we want to reach
extern int32_t target_altitude;
//This is the interim value which is feeded into the althold controller
extern int32_t alt_to_hold;
extern uint32_t alt_change_timer;
extern int8_t alt_change_flag;
extern uint32_t alt_change;
extern int16_t jump_times; //How many loops do we have to do (alt/100 from mission step) -10 means not used jet, -1 unlimited
extern uint8_t land_detect; //land detector variable
// ************************
// mission step structure
// ************************
extern mission_step_struct mission_step;
//possible action codes for a mission step
#define MISSION_WAYPOINT 1 //Set waypoint
#define MISSION_HOLD_UNLIM 2 //Poshold unlimited
#define MISSION_HOLD_TIME 3 //Hold for a predetermined time
#define MISSION_RTH 4 //Return to HOME
#define MISSION_SET_POI 5 //Set POINT of interest
#define MISSION_JUMP 6 //Jump to the given step (#times)
#define MISSION_SET_HEADING 7 //Set heading to a given orientation (parameter 1 is the waym 0-359 degree
#define MISSION_LAND 8 //Land at the given position
#define MISSION_FLAG_END 0xA5 //Flags that this is the last step
#define MISSION_FLAG_CRC_ERROR 0xFE //Returned WP had an EEPROM CRC error
#define MISSION_FLAG_HOME 0x01 //Returned WP is the home position
#define MISSION_FLAG_HOLD 0x02 //Returned WP is the hold position
#define MISSION_FLAG_DO_LAND 0x20 //Land when reached desired point (used in RTH)
#define MISSION_FLAG_NAV_IN_PROG 0xff //Navigation is in progress, returned wp is home
#define LAT 0
#define LON 1
extern int16_t nav[2];
#endif
// default POSHOLD control gains
#define POSHOLD_P .15
#define POSHOLD_I 0.0
#define POSHOLD_IMAX 20 // degrees
#define POSHOLD_RATE_P 3.4
#define POSHOLD_RATE_I 0.14 // Wind control
#define POSHOLD_RATE_D 0.053 // try 2 or 3 for POSHOLD_RATE 1
#define POSHOLD_RATE_IMAX 20 // degrees
// default Navigation PID gains
#define NAV_P 2.5
#define NAV_I 0.33 // Wind control
#define NAV_D 0.083 //
#define NAV_IMAX 20 // degrees
// *************************************** end GPS common variables and defines ******************************************************************
extern volatile uint8_t spekFrameFlags;
extern volatile uint32_t spekTimeLast;
extern uint8_t spekFrameDone;
#if defined(OPENLRSv2MULTI)
extern uint8_t pot_P,pot_I; // OpenLRS onboard potentiometers for P and I trim or other usages
#endif
// **********************
//Automatic ACC Offset Calibration
// **********************
#if defined(INFLIGHT_ACC_CALIBRATION)
extern uint16_t InflightcalibratingA;
extern int16_t AccInflightCalibrationArmed;
extern uint16_t AccInflightCalibrationMeasurementDone;
extern uint16_t AccInflightCalibrationSavetoEEProm;
extern uint16_t AccInflightCalibrationActive;
#endif
#if defined(ARMEDTIMEWARNING)
extern uint32_t ArmedTimeWarningMicroSeconds;
#endif
#if defined(THROTTLE_ANGLE_CORRECTION)
extern int16_t throttleAngleCorrection;
extern int8_t cosZ;
#endif
void annexCode();
void go_disarm();
#endif /* MULTIWII_H_ */