Switching control method and equipment for launch flight state of aircraft
The invention discloses an aircraft launch flight state switching control method and equipment thereof. According to the control method, in the initial launching stage of the aircraft, a first-stage booster is controlled to be in a working state, and the first-stage booster propels the aircraft to l...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | The invention discloses an aircraft launch flight state switching control method and equipment thereof. According to the control method, in the initial launching stage of the aircraft, a first-stage booster is controlled to be in a working state, and the first-stage booster propels the aircraft to lift off; when the first-stage booster is separated from the aircraft, the first-stage booster is switched from a working state to a dormant state, the second-stage booster is in a working state, and the second-stage booster propels the aircraft to lift off; when the separation of the second-stage booster and the aircraft is completed, the second-stage booster is switched from the working state to the dormant state, the third-stage booster is in the working state, and the third-stage booster propels the aircraft to lift off. And the automatic and real-time monitoring of the variation trend of the degradation of the control system can be realized.
本公开的飞行器发射飞行状态的切换控制方法及其设备。本该控制方法通过在所述飞行器发射初始阶段,控制一级助推器处于工作状态,所述一级助推器推进飞 |
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