flight_altitudehold_unittest.cc File Reference

#include <stdint.h>
#include <stdbool.h>
#include <limits.h>
#include <platform.h>
#include "build_config.h"
#include "debug.h"
#include "common/axis.h"
#include "common/maths.h"
#include "drivers/sensor.h"
#include "drivers/accgyro.h"
#include "sensors/acceleration.h"
#include "sensors/barometer.h"
#include "rx/rx.h"
#include "flight/mixer.h"
#include "flight/anglerate.h"
#include "flight/altitudehold.h"
#include "config/config.h"
#include "config/rc_controls.h"
#include "config/altitudehold.h"
#include "config/mixer.h"
#include "unittest_macros.h"
#include "gtest/gtest.h"

Include dependency graph for flight_altitudehold_unittest.cc:

Data Structures
struct	inclinationExpectation_s

Macros
#define	BARO
#define	DOWNWARDS_THRUST   true
#define	UPWARDS_THRUST   false

Typedefs
typedef struct inclinationExpectation_s	inclinationExpectation_t

Functions
bool	isThrustFacingDownwards (union attitude_euler_angles *attitude)
uint16_t	calculateTiltAngle (union attitude_euler_angles *attitude)
bool	rcModeIsActive (boxId_e modeId)
int16_t	rc_get_channel_value (uint8_t id)
void	rc_set_channel_value (uint8_t id, int16_t value)
float	imu_get_velocity_integration_time (struct imu *self)
float	imu_get_est_vertical_vel_cms (struct imu *self)
void	imu_reset_velocity_estimate (struct imu *self)
float	imu_get_avg_vertical_accel_cmss (struct imu *self)
int16_t	imu_get_roll_dd (struct imu *self)
int16_t	imu_get_pitch_dd (struct imu *self)
void	gyroUpdate (void)
bool	sensors (uint32_t mask)
void	updateAccelerationReadings (rollAndPitchTrims_t *rollAndPitchTrims)
void	imuResetAccelerationSum (void)
uint32_t	micros (void)
bool	isBaroCalibrationComplete (void)
void	performBaroCalibrationCycle (void)
int32_t	baroCalculateAltitude (void)

Variables
struct imu	default_imu
uint32_t	rcModeActivationMask
int16_t	rcCommand [4]
int16_t	rcData [RX_MAX_SUPPORTED_RC_CHANNELS]
uint32_t	accTimeSum
int	accSumCount
float	accVelScale
int32_t	BaroAlt
int16_t	debug [DEBUG16_VALUE_COUNT]
uint8_t	stateFlags
uint16_t	flightModeFlags
uint8_t	armingFlags
int32_t	sonarAlt
int16_t	sonarCfAltCm
int16_t	sonarMaxAltWithTiltCm

Macro Definition Documentation

#define BARO

#define DOWNWARDS_THRUST   true

#define UPWARDS_THRUST   false

Typedef Documentation

typedef struct inclinationExpectation_s inclinationExpectation_t

Function Documentation

int32_t baroCalculateAltitude

(

void

)

uint16_t calculateTiltAngle

(

union attitude_euler_angles *

attitude

)

void gyroUpdate

(

void

)

void imuResetAccelerationSum

(

void

)

bool isBaroCalibrationComplete

(

void

)

bool isThrustFacingDownwards

(

union attitude_euler_angles *

attitude

)

uint32_t micros

(

void

)

void performBaroCalibrationCycle

(

void

)

int16_t rc_get_channel_value

(

uint8_t

id

)

void rc_set_channel_value	(	uint8_t	id,
		int16_t	value
	)

bool rcModeIsActive

(

boxId_e

modeId

)

bool sensors

(

uint32_t

mask

)

void updateAccelerationReadings

(

rollAndPitchTrims_t *

rollAndPitchTrims

)

Variable Documentation

int accSumCount

uint32_t accTimeSum

float accVelScale

uint8_t armingFlags

int32_t BaroAlt

int16_t debug[DEBUG16_VALUE_COUNT]

struct imu default_imu

uint16_t flightModeFlags

int16_t rcCommand[4]

int16_t rcData[RX_MAX_SUPPORTED_RC_CHANNELS]

uint32_t rcModeActivationMask

int32_t sonarAlt

int16_t sonarCfAltCm

int16_t sonarMaxAltWithTiltCm

uint8_t stateFlags