It had not been explored which real-time magnitude can meet the requirement of the simulation object in computer simulation system. Taking time delay into consideration, the influence of time delay on the stability of the low-altitude and low-speed small Unmanned Aircraft Systems (UAS) flight control system had been analyzed and the real-time magnitude of the miniature hardware-in-loop (HIL) simulation system was determined. Then a miniature HIL simulation system of the UAS flight control system was designed to prove the real-time magnitude feasibility. The result shows the real-time magnitude by time delay analysis can meet the requirements of flight control system.
Design and Verification the Simulation System of UAS Flight Control Considering the Effects of Time Delay
Applied Mechanics and Materials ; 278-280 ; 1746-1753
2013-01-11
8 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Robust Flight Control System Design Verification & Validation for Launchers
British Library Conference Proceedings | 2012
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