Stability region of closed-loop pilot-vehicle system for fly-by-wire aircraft with limited actuator rate

Other literature type English OPEN
Ying-hui, Li; Liang, Qu; Hao-jun, Xu; Qi-meng, Cao;
(2017)
  • Publisher: Faculty of Engineering/Faculty of Civil Engineering, University of Rijeka
  • Journal: Engineering Review : Međunarodni časopis namijenjen publiciranju originalnih istraživanja s aspekta analize konstrukcija, materijala i novih tehnologija u području strojarstva, brodogradnje, temeljnih tehničkih znanosti, elektrotehnike, računarstva i građevinarstva,volume 37,issue 3 (issn: 1330-9587, eissn: 1849-0433)
  • Publisher copyright policies & self-archiving
  • Subject: pilot induced oscillation; rate limited actuator; closed-loop pilot-vehicle system; stability regions; linear matrix inequality

The category-II PIO (Pilot Induced Oscillations) caused by actuator rate limitation of fly-by-wire airplanes will badly threaten the flight safety. The stability regions of closed-loop pilot-vehicle (CLPV) system with rate limited actuator were studied in this paper to ... View more
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