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驾驶员诱发振荡的研究
引用本文:陈廷楠,徐浩军.驾驶员诱发振荡的研究[J].航空学报,1991,12(8):339-344.
作者姓名:陈廷楠  徐浩军
作者单位:空军工程学院 (陈廷楠),空军工程学院(徐浩军)
摘    要: 本文根据驾驶员诱发振荡的实质,从闭环控制理论出发,提出了人-机系统数学模型,并在时域内进行了计算。以某歼击教练机为例,与频域法一起作了对比研究。结果表明,时域计算方法不仅直观,物理意义强,而且可以考虑众多的非线性因素,结果可能较为可靠。

关 键 词:驾驶员诱发振荡  飞行品质  人-机系统  

THE RESEARCH ON PILOT INDUCED OSCILLATION
Air Force College of Engineering Chen Tingnan and Xu Haojun.THE RESEARCH ON PILOT INDUCED OSCILLATION[J].Acta Aeronautica et Astronautica Sinica,1991,12(8):339-344.
Authors:Air Force College of Engineering Chen Tingnan and Xu Haojun
Institution:Air Force College of Engineering Chen Tingnan and Xu Haojun
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.
Keywords:polit induced oscillation  flying-quality  pilot-plane system  
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