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[7] -80
-40
on pitch angle stabilization
0 500 1 000 1 500
Blue: azimuth angle
Blue: azimuth angle
Sampling time: 0.002 s
move and pitch angle move separately
Fig.4 The overall effect of infrared sight
0
Fig.2 Before decoupling, impact of azimuth sinusoidal move
40
axis stabilization system
Chiang R Y，Safonov M G. A fixed controller for a super maneuverable fighter performing the Herbst maneuver [J].Automatica(S0254-4156)，1993，29(1)：111-127.
Code value: 0.00137°
80
on pitch angle stabilization
Sampling time: 0.002 s
Red: pitching angle
143
0
-80
40
80
Fig.5 After decoupling,the effect of azimuth angle
Red: pitching angle
Fig.3 After decoupling, impact of azimuth sinusoidal move
-40
0 500 1 000 1 500
Code value: 0.00137°
[8] Chan W，Anderson R. Decoupling synchronization from local control for efficient symbolic model checking of state charts[C]//Proceedings of the 1999 International Conference onSoftware Engineering(ICSE99)，Los Angeles, California, United States，May 16-22，1999：142-151.
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