Study on Pilot Transfer Function Model Gain of Closed-Loop Pilot-Vehicle System

Abstract:

Based on the analysis of pilot handling behavior characteristics, this paper establishes the pilot transfer function model. According to the characteristics of closed-loop pilot-vehicle system and the relationship between pilot and flight quality, the specific calculation method of pilot model steady state gain was given. Take the aircraft roll angle manipulation for example, and simulate the pilot's manipulation of aircraft of dynamic process. The results show that: the pilot model steady state gain calculation method is simple and feasible, and have a certain reference value for the analysis of closed-loop pilot-vehicle system.

• Periodical: Advanced Materials Research (Volumes 706-708)
• Pages: 1038-1041
• DOI: https://doi.org/10.4028/www.scientific.net/AMR.706-708.1038
• Online since: June 2013
• Authors: Lin Li, Jun Xu, Fu Lei Zheng
• Keywords: Closed-Loop Pilot-Vehicle System, Pilot Model, Simulation

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DOI: 10.1080/00423119308969025