Multi-rotor aircraft control method

The invention relates to a multi-rotor aircraft control method, which comprises the following steps: acquiring a space trajectory instruction Pd and an attitude angle instruction theta d of a multi-rotor aircraft, and a flight trajectory coordinate P and an attitude vector theta at a t moment; a tra...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	CHENG CHUN, XU DONGQING, WU WANQI, HUANG WENSHENG, ZHANG HONGGAN, SHEN HONGQI
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	CONTROLLING PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
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