导航
ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1991, Vol. 12 ›› Issue (8): 339-344.
• 论文 • Previous Articles Next Articles
Chen Tingnan, Xu Haojun
Received:
Revised:
Online:
Published:
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
Chen Tingnan;Xu Haojun. THE RESEARCH ON PILOT INDUCED OSCILLATION[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1991, 12(8): 339-344.
0 / / Recommend
Add to citation manager EndNote|Reference Manager|ProCite|BibTeX|RefWorks
URL: https://hkxb.buaa.edu.cn/EN/
https://hkxb.buaa.edu.cn/EN/Y1991/V12/I8/339