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#ifndef _CONFIGURATION_H |
#define _CONFIGURATION_H |
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#include <inttypes.h> |
#include <avr/io.h> |
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#define MAX_CHANNELS 10 |
#define MAX_MOTORS 12 |
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// bitmask for VersionInfo_t.HardwareError[0] |
#define FC_ERROR0_GYRO_PITCH 0x01 |
#define FC_ERROR0_GYRO_ROLL 0x02 |
#define FC_ERROR0_GYRO_YAW 0x04 |
#define FC_ERROR0_ACC_X 0x08 |
#define FC_ERROR0_ACC_Y 0x10 |
#define FC_ERROR0_ACC_Z 0x20 |
#define FC_ERROR0_PRESSURE 0x40 |
#define FC_ERROR1_RES0 0x80 |
// bitmask for VersionInfo_t.HardwareError[1] |
#define FC_ERROR1_I2C 0x01 |
#define FC_ERROR1_BL_MISSING 0x02 |
#define FC_ERROR1_SPI_RX 0x04 |
#define FC_ERROR1_PPM 0x08 |
#define FC_ERROR1_MIXER 0x10 |
#define FC_ERROR1_RES1 0x20 |
#define FC_ERROR1_RES2 0x40 |
#define FC_ERROR1_RES3 0x80 |
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typedef struct { |
uint8_t gyroQuadrant; |
uint8_t accQuadrant; |
uint8_t imuReversedFlags; |
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uint8_t gyroPIDFilterConstant; |
uint8_t gyroDWindowLength; |
uint8_t gyroDFilterConstant; |
uint8_t accFilterConstant; |
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uint8_t zerothOrderCorrection; |
uint8_t rateTolerance; |
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uint8_t gyroActivityDamping; |
uint8_t driftCompDivider; // 1/k (Koppel_ACC_Wirkung) |
uint8_t driftCompLimit; // limit for gyrodrift compensation |
} IMUConfig_t; |
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extern IMUConfig_t IMUConfig; |
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typedef struct { |
uint8_t P; |
uint8_t I; |
uint8_t D; |
} PID_t; |
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typedef struct { |
uint8_t P; |
uint8_t I; |
uint8_t D; |
uint8_t iMax; |
} PIDIM_t; |
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typedef enum { |
FLIGHT_MODE_NONE, |
FLIGHT_MODE_MANUAL, |
FLIGHT_MODE_RATE, |
FLIGHT_MODE_ANGLES |
} FlightMode_t; |
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#define CONTROL_SERVO_REVERSE_ELEVATOR 1 |
#define CONTROL_SERVO_REVERSE_AILERONS 2 |
#define CONTROL_SERVO_REVERSE_RUDDER 4 |
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typedef struct { |
uint8_t SWMajor; |
uint8_t SWMinor; |
uint8_t protoMajor; |
uint8_t protoMinor; |
uint8_t SWPatch; |
uint8_t hardwareErrors[5]; |
}__attribute__((packed)) VersionInfo_t; |
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extern VersionInfo_t versionInfo; |
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typedef struct { |
// IMU stuff: |
PID_t gyroPID[3]; |
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// Control |
/* P */uint8_t externalControl; |
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// Output and servo |
/*PMM*/uint8_t output0Timing; |
/*PMM*/uint8_t output1Timing; |
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uint8_t servoManualControl[2]; |
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/* P */uint8_t userParams[8]; |
} DynamicParams_t; |
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extern volatile DynamicParams_t dynamicParams; |
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typedef struct { |
uint8_t sourceIdx, targetIdx; |
uint8_t min, max; |
} MMXLATION; |
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/* |
typedef struct { |
uint8_t sourceIdx, targetIdx; |
} XLATION; |
*/ |
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typedef struct { |
uint8_t channels[MAX_CHANNELS]; |
} channelMap_t; |
extern channelMap_t channelMap; |
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typedef struct { |
int16_t offsets[3]; |
} sensorOffset_t; |
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typedef struct { |
uint8_t manualControl; |
uint8_t stabilizationFactor; |
uint8_t minValue; |
uint8_t maxValue; |
uint8_t flags; |
} servo_t; |
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#define SERVO_STABILIZATION_REVERSE 1 |
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typedef struct { |
uint8_t bitmask; |
uint8_t timing; |
} output_flash_t; |
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// values above 250 representing poti1 to poti4 |
typedef struct { |
// Global bitflags |
uint8_t bitConfig; // see upper defines for bitcoding |
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// Control |
PIDIM_t gyroPID[3]; |
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uint8_t stickIElevator; |
uint8_t stickIAilerons; |
uint8_t stickIRudder; |
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uint8_t externalControl; // for serial Control |
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uint8_t IFactor; |
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uint8_t batteryVoltageWarning; |
uint8_t emergencyThrottle; |
uint8_t emergencyFlightDuration; |
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// Airspeed |
uint8_t airspeedCorrection; |
uint8_t isFlyingThreshold; |
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// Servos |
uint8_t controlServosReverse; |
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uint8_t servoCount; |
uint8_t servoManualMaxSpeed; |
servo_t servoConfigurations[2]; // [PITCH, ROLL] |
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// Outputs |
output_flash_t outputFlash[2]; |
uint8_t outputDebugMask; |
uint8_t outputFlags; |
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// User params |
uint8_t userParams[8]; |
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// Name |
char name[12]; |
} ParamSet_t; |
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extern ParamSet_t staticParams; |
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// bit mask for staticParams.bitConfig |
#define CFG_GYRO_SATURATION_PREVENTION (1<<0) |
#define CFG_USE_AIRSPEED_PID (1<<1) |
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#define IMU_REVERSE_GYRO_PR (1<<0) |
#define IMU_REVERSE_GYRO_YAW (1<<1) |
#define IMU_REVERSE_ACC_XY (1<<2) |
#define IMU_REVERSE_ACC_Z (1<<3) |
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#define ATMEGA644 0 |
#define ATMEGA644P 1 |
#define SYSCLK F_CPU |
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// Not really a part of configuration, but LEDs and HW s test are the same. |
#define RED_OFF {PORTD &=~(1<<PORTD6);} |
#define RED_ON {PORTD |= (1<<PORTD6);} |
#define RED_FLASH PORTD ^= (1<<PORTD6) |
#define GRN_OFF {PORTD &=~(1<<PORTD7);} |
#define GRN_ON {PORTD |= (1<<PORTD7);} |
#define GRN_FLASH PORTD ^= (1<<PORTD7) |
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// Mixer table |
#define MIX_THROTTLE 0 |
#define MIX_PITCH 1 |
#define MIX_ROLL 2 |
#define MIX_YAW 3 |
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#define VARIABLE_COUNT 8 |
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extern int16_t variables[VARIABLE_COUNT]; // The "Poti"s. |
extern uint8_t CPUType; |
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extern volatile uint16_t isFlying; |
extern FlightMode_t currentFlightMode; |
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void IMUConfig_default(void); |
void channelMap_default(void); |
void paramSet_default(uint8_t setnumber); |
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void configuration_setFlightParameters(uint8_t newFlightMode); |
void configuration_applyVariablesToParams(void); |
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void setCPUType(void); |
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// Called after a change in configuration parameters, as a hook for modules to take over changes. |
void configuration_paramSetDidChange(void); |
#endif // _CONFIGURATION_H |