Actuator Rate Limiting Boundary Based on Pilot-vehicleSystem Stability Requirements
Actuator rate limiting is the primary course of aircraft pilot coupling(APC) for fly-by-wire(FBW) aircraft. The actuator rate limiting is modeled by describing function. The relationships between actuator rate limiting, APC onset frequency and PVS closed-loop stability are analyzed. On the basis of...
Main Authors: | , , |
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Format: | Article |
Language: | zho |
Published: |
Editorial Department of Advances in Aeronautical Science and Engineering
2018-02-01
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Series: | Hangkong gongcheng jinzhan |
Subjects: | |
Online Access: | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2017122?st=article_issue |