Quadrotor unmanned aerial vehicle attitude control method based on rapid nonsingular terminal sliding mode

The invention provides a quadrotor unmanned aerial vehicle attitude control method based on a rapid nonsingular terminal sliding mode. The method comprises the following steps: constructing a mathematical model of a quadrotor unmanned aerial vehicle; designing an integral terminal sliding mode funct...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	WANG YURONG, CHEN SHUSHENG, CHE SHIQI, ZOU XU, NAKAYASU, YANG HUA
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	CONTROLLING PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
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