Method for designing maneuvering simulation control law of a hybrid-configuration fixed-wing unmanned aerial vehicle

The invention discloses a method for designing a maneuvering simulation control law of a hybrid-configuration fixed-wing unmanned aerial vehicle. The method comprises the following steps: establishing a six-degree-of-freedom nonlinear mathematical model of the fixed-wing unmanned aerial vehicle; bui...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	GUAN XIANGMIN, LYU RENLI, WANG MAOLIN
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING FUNCTIONAL ELEMENTS OF SUCH SYSTEMS MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PHYSICS REGULATING
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