1
0
Fork 0
mirror of https://github.com/betaflight/betaflight.git synced 2025-07-24 00:35:39 +03:00
betaflight/src/main/flight/imu.h
Martin Budden 152c594151 Code tidy
2017-04-11 19:05:54 +01:00

84 lines
2.5 KiB
C

/*
* This file is part of Cleanflight.
*
* Cleanflight is free software: you can redistribute it and/or modify
* it under the terms of the GNU General Public License as published by
* the Free Software Foundation, either version 3 of the License, or
* (at your option) any later version.
*
* Cleanflight is distributed in the hope that it will be useful,
* but WITHOUT ANY WARRANTY; without even the implied warranty of
* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
* GNU General Public License for more details.
*
* You should have received a copy of the GNU General Public License
* along with Cleanflight. If not, see <http://www.gnu.org/licenses/>.
*/
#pragma once
#include "common/axis.h"
#include "common/time.h"
#include "config/parameter_group.h"
// Exported symbols
extern uint32_t accTimeSum;
extern int accSumCount;
extern float accVelScale;
extern int32_t accSum[XYZ_AXIS_COUNT];
typedef union {
int16_t raw[XYZ_AXIS_COUNT];
struct {
// absolute angle inclination in multiple of 0.1 degree 180 deg = 1800
int16_t roll;
int16_t pitch;
int16_t yaw;
} values;
} attitudeEulerAngles_t;
extern attitudeEulerAngles_t attitude;
typedef struct accDeadband_s {
uint8_t xy; // set the acc deadband for xy-Axis
uint8_t z; // set the acc deadband for z-Axis, this ignores small accelerations
} accDeadband_t;
typedef struct imuConfig_s {
uint16_t dcm_kp; // DCM filter proportional gain ( x 10000)
uint16_t dcm_ki; // DCM filter integral gain ( x 10000)
uint8_t small_angle;
uint8_t acc_unarmedcal; // turn automatic acc compensation on/off
accDeadband_t accDeadband;
} imuConfig_t;
PG_DECLARE(imuConfig_t, imuConfig);
typedef struct imuRuntimeConfig_s {
float dcm_ki;
float dcm_kp;
uint8_t acc_unarmedcal;
uint8_t small_angle;
accDeadband_t accDeadband;
} imuRuntimeConfig_t;
void imuConfigure(uint16_t throttle_correction_angle);
float getCosTiltAngle(void);
void imuUpdateAttitude(timeUs_t currentTimeUs);
int16_t calculateThrottleAngleCorrection(uint8_t throttle_correction_value);
void imuResetAccelerationSum(void);
void imuInit(void);
#ifdef SIMULATOR_BUILD
void imuSetAttitudeRPY(float roll, float pitch, float yaw); // in deg
void imuSetAttitudeQuat(float w, float x, float y, float z);
#if defined(SIMULATOR_IMU_SYNC)
void imuSetHasNewData(uint32_t dt);
#endif
#endif