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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1991, Vol. 12 ›› Issue (8): 339-344.

• 论文 • Previous Articles     Next Articles

THE RESEARCH ON PILOT INDUCED OSCILLATION

Chen Tingnan, Xu Haojun   

  1. Air Force College of Engineering
  • Received:1989-12-01 Revised:1990-09-01 Online:1991-08-25 Published:1991-08-25

Abstract: According to the essence of Pilot Induced Oscillation (PIO) and the theory of Closed-loop control, the mathematical model of Pilot-Plane system is set up. Take a fighter trainer as an example, its PIOs are calculated in time-domain, and their results are compared with those obtained from the frequency-domain method. The results show that time-domain method is not only visualized but also is very clear in physical meaning. Moreover a lot of nonlinear elements are also easy to be considered. Its result may be more reliable.

Key words: polit induced oscillation, flying-quality, pilot-plane system