Guidance method and guidance system applied to laser/satellite composite aircraft

The invention discloses a guidance method and guidance system applied to a laser/satellite composite aircraft, and the method comprises the steps: employing a proportional guidance law for a middle guidance section of the aircraft, employing a re-compensation proportional guidance law for a terminal...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	WANG WEI, WANG WEIBIN, NAN YUXIANG, LIN DEFU, GENG BAOKUI, WANG YUCHEN, WANG LUQIANG
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	CONTROLLING PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
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