Design and Verification the Simulation System of UAS Flight Control Considering the Effects of Time Delay

Abstract:

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.

• Periodical: Applied Mechanics and Materials (Volumes 278-280)
• Pages: 1746-1753
• DOI: https://doi.org/10.4028/www.scientific.net/AMM.278-280.1746
• Online since: January 2013
• Authors: Sheng Yi Yang, Sheng Jing Tang, Chao Liu, Jie Guo
• Keywords: Flight Control System, HIL Simulation, Time Delay, UAS

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