Research on Attitude Measurement Method of Special Aircraft Using Geomagnetic Sensor/Gyroscope Based on UKF

Table 1

Initial conditions of a simulation experiment.

Flight time (s)	Sampling interval (s)	Initial velocity (m/s)	Initial pitch angle (°)
87.5	0.1	897	45
Initial yaw angle (°)	Flight distance (m)	The highest position of flight path (m)	Initial spin velocity (r/s)
0	27126.4	9377	300