2012-11-14 12:10:15 -04:00
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#ifndef __AP_AHRS_HIL_H__
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#define __AP_AHRS_HIL_H__
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2010-12-10 06:17:27 -04:00
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2012-03-11 05:00:06 -03:00
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class AP_AHRS_HIL : public AP_AHRS
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{
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public:
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2012-08-21 23:19:51 -03:00
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// Constructors
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2012-11-14 12:10:15 -04:00
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AP_AHRS_HIL(AP_InertialSensor *ins, GPS *&gps) : AP_AHRS(ins, gps) {}
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2012-08-21 23:19:51 -03:00
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// Accessors
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Vector3f get_gyro(void) {
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return _omega;
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}
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Matrix3f get_dcm_matrix(void) {
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Matrix3f m;
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m.from_euler(roll, pitch, yaw);
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return m;
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}
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// Methods
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2012-11-14 12:10:15 -04:00
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void update(void) {
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_ins->update();
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2012-08-21 23:19:51 -03:00
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}
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2012-09-15 05:47:18 -03:00
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2012-11-14 12:10:15 -04:00
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void setHil(float roll, float pitch, float yaw,
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float rollRate, float pitchRate, float yawRate);
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2012-08-21 23:19:51 -03:00
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// return the current estimate of the gyro drift
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Vector3f get_gyro_drift(void) {
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return Vector3f(0,0,0);
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}
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// reset the current attitude, used on new IMU calibration
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void reset(bool recover_eulers=false) {
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}
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float get_error_rp(void) {
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return 0;
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}
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float get_error_yaw(void) {
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return 0;
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}
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2011-07-30 17:34:23 -03:00
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2010-12-10 06:17:27 -04:00
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private:
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2012-08-21 23:19:51 -03:00
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Vector3f _omega;
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2010-12-10 06:17:27 -04:00
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};
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2012-11-14 12:10:15 -04:00
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#endif // __AP_AHRS_HIL_H__
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