ardupilot/libraries/AP_AHRS/AP_AHRS.cpp

69 lines
2.1 KiB
C++

/*
APM_AHRS.cpp
This library is free software; you can redistribute it and/or
modify it under the terms of the GNU Lesser General Public License
as published by the Free Software Foundation; either version 2.1
of the License, or (at your option) any later version.
*/
#include <FastSerial.h>
#include <AP_AHRS.h>
// table of user settable parameters
const AP_Param::GroupInfo AP_AHRS::var_info[] PROGMEM = {
// index 0 and 1 are for old parameters that are no longer used
// @Param: GPS_GAIN
// @DisplayName: AHRS GPS gain
// @Description: This controls how how much to use the GPS to correct the attitude
// @Range: 0.0 1.0
// @Increment: .01
AP_GROUPINFO("GPS_GAIN", 2, AP_AHRS, gps_gain, 1.0),
// @Param: GPS_USE
// @DisplayName: enable/disable use of GPS for position estimation
// @Description: This controls how how much to use the GPS to correct the attitude. This is for testing the dead-reckoning code
// @User: Advanced
AP_GROUPINFO("GPS_USE", 3, AP_AHRS, _gps_use, 1),
// @Param: YAW_P
// @DisplayName: Yaw P
// @Description: This controls the weight the compass has on the overall heading
// @Range: 0 .4
// @Increment: .01
AP_GROUPINFO("YAW_P", 4, AP_AHRS, _kp_yaw, 0.4),
// @Param: RP_P
// @DisplayName: AHRS RP_P
// @Description: This controls how fast the accelerometers correct the attitude
// @Range: 0 .4
// @Increment: .01
AP_GROUPINFO("RP_P", 5, AP_AHRS, _kp, 0.4),
AP_GROUPEND
};
// get pitch rate in earth frame, in radians/s
float AP_AHRS::get_pitch_rate_earth(void)
{
Vector3f omega = get_gyro();
return cos(roll) * omega.y - sin(roll) * omega.z;
}
// get roll rate in earth frame, in radians/s
float AP_AHRS::get_roll_rate_earth(void) {
Vector3f omega = get_gyro();
return omega.x + tan(pitch)*(omega.y*sin(roll) + omega.z*cos(roll));
}
// return airspeed estimate if available
bool AP_AHRS::airspeed_estimate(float *airspeed_ret)
{
if (_airspeed && _airspeed->use()) {
*airspeed_ret = _airspeed->get_airspeed();
return true;
}
return false;
}