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@ -359,8 +359,8 @@ struct stateSample { |
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Quaternion quat_nominal; // quaternion defining the rotaton from earth to body frame
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Quaternion quat_nominal; // quaternion defining the rotaton from earth to body frame
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Vector3f vel; // NED velocity in earth frame in m/s
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Vector3f vel; // NED velocity in earth frame in m/s
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Vector3f pos; // NED position in earth frame in m
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Vector3f pos; // NED position in earth frame in m
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Vector3f gyro_bias; // gyro bias estimate in rad/s
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Vector3f gyro_bias; // delta angle bias estimate in rad
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Vector3f accel_bias; // accelerometer bias estimate in m/s
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Vector3f accel_bias; // delta velocity bias estimate in m/s
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Vector3f mag_I; // NED earth magnetic field in gauss
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Vector3f mag_I; // NED earth magnetic field in gauss
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Vector3f mag_B; // magnetometer bias estimate in body frame in gauss
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Vector3f mag_B; // magnetometer bias estimate in body frame in gauss
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Vector2f wind_vel; // wind velocity in m/s
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Vector2f wind_vel; // wind velocity in m/s
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