Governed by: Ministry of Industry and Information Technology of the People's Republic of China
Sponsored by: Northwestern Polytechnical University  Chinese Society Aeronautics and Astronautics
Address: Aviation Building,Youyi Campus, Northwestern Polytechnical University
Research on two kinds of approach power compensator system of carrier-based aircraft based on Hdot command
Author:
Affiliation:

1.Naval Academy;2.China

Clc Number:

TP273,V249

Fund Project:

China Postdoctoral Science Foundation

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    Abstract:

    The use of power compensation system can greatly reduce the burden of pilot control, and can improve the dynamic response speed and control accuracy. This article focuses on the research of two carrier-based aircraftpower compensation control systems. Firstly, based on the Hdot command, the two approach power compensation systems of angle of attack and speed control were designed. Secondly, the simulation analysis was carried out for the two approach power compensation control systems, and the approach dynamic compensation response of the two compensation systems in the case of airwake disturbance was further analyzed, and their basic principles were analyzed through the simulation results: The ability of the angle of attack power compensation system to stabilize the angle of attack is greater than that of the constant speed, and the trajectory control is also faster than the constant speed power compensation system.

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ZHANG Yang, ZHOU Yi, YAN Xianrong, YIN Dawei, QIAN Guohong. Research on two kinds of approach power compensator system of carrier-based aircraft based on Hdot command[J]. Advances in Aeronautical Science and Engineering,2022,13(4):140-146

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History
  • Received:July 04,2021
  • Revised:November 28,2021
  • Adopted:January 18,2022
  • Online: March 25,2022
  • Published: