High-dynamic compensation guidance control system and method aiming at high-speed maneuvering target
The invention discloses a high-dynamic compensation guidance control system and method aiming at a high-speed maneuvering target. The system comprises a measuring module (1), a processing module (2) and an execution module (3). The measuring module (1) is used for measuring the relative position inf...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | The invention discloses a high-dynamic compensation guidance control system and method aiming at a high-speed maneuvering target. The system comprises a measuring module (1), a processing module (2) and an execution module (3). The measuring module (1) is used for measuring the relative position information of a high-dynamic air vehicle and the high-speed maneuvering target and the posture information of the high-dynamic air vehicle in real time. The processing module (2) is used for acquiring a rudder deflection command signal according to the information measured by the measuring module in real time. The execution module (3) is used for receiving the rudder deflection command signal acquired by the processing module and converting the signal into the signal form needed by a steering engine. According to the system, the real-time relative position information of the air vehicle and the target is acquired through an active radar, the posture information of the air vehicle is acquired through an MEMS gyro and |
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