Research Article

Attitude Measurement of Special Aircraft Based on Geomagnetic and Angular Velocity Sensors

Table 1

Simulation parameters.

Flight time (s)Sampling interval (s)Initial pitch angle (°)Initial yaw angle (°)Initial flight speed (m/s)

87.50.14575897
Flight distance (m)Highest position of flight path (m)Magnetic inclination (°)Magnetic declination (°)Magnetic field intensity (nT)
27126.49377-48.17°-2.32°50986.1