Attitude control test device for six-degree-of-freedom unmanned aerial vehicle

The invention provides an attitude control test device for a six-degree-of-freedom unmanned aerial vehicle. The attitude control test device comprises a base, a frame, a three-degree-of-freedom joint, a first rotating device, a first revolute pair, a second rotating device, a second revolute pair, a...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	WANG YINGCHUN, ZHANG BAOMIN, ZHAO XUN, WANG HONGYU, LIU LING, DIAO QIZHUO, TIAN ZUOHUA
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR PERFORMING OPERATIONS TRANSPORTING
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