Pilot-Induced Oscillation Analysis with Actuator Rate Limiting and Feedback Control Loop

Ryoji Katayanagi

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Pilot-Induced Oscillation Analysis with Actuator Rate Limiting and Feedback Control Loop

机译：具有执行器速率限制和反馈控制环的飞行员感应振荡分析

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摘要

Fully-developed pilot-induced oscillation(PIO)is animportant issue to be solved in the development of modern fly-by-wire flight control systems. A new method is presented to analyze the limit cycle phenomenon of the PIO, including the effects of actuator rate limiting and feedback control. By using describing function method, the frequency and the amplitude of the PIO limit cycle are obtained analytically. It is shown that the predictions obtained with this present method closely match results of the simulation.

机译：全面发展的飞行员感应振荡（PIO）是现代电传操纵飞行控制系统开发中要解决的重要问题。提出了一种新的方法来分析PIO的极限循环现象，包括执行器速率限制和反馈控制的影响。通过使用描述函数法，可以解析得出PIO极限周期的频率和幅度。结果表明，用本方法获得的预测结果与模拟结果非常吻合。

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《Transactions of the Japan society for aeronautical and space sciences》 |2001年第143期|p.46-51|共6页
作者
Ryoji Katayanagi;
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作者单位

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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
中图分类航空;
关键词
flight control system; pilot-induced oscillation; actuator rate limiting;

机译：飞行控制系统;飞行员引起的振荡执行器速率限制;

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专利

1. pilot-induced oscillation analysis with Actuator rate limiting and feedback control loop [J] . Ryoji katayanagl Transactions of the Japan society for aeronautical and space sciences . 2001,第143期

机译：具有执行器速率限制和反馈控制回路的先导感应振荡分析
2. Model Predictive Controller Design to Suppress Rate-Limiter-Based Pilot-Induced Oscillations [J] . Xue-hui Liang, Katsuhiko Yamada, Noboru Sakamoto, Transactions of the Japan society for aeronautical and space sciences . 2007,第166期

机译：模型预测控制器设计可抑制基于速率限制器的飞行员引起的振荡
3. A hormone-dependent feedback-loop controls androgen receptor levels by limiting MID1, a novel translation enhancer and promoter of oncogenic signaling [J] . Andrea K?hler, ümmühan Demir, Eva Kickstein, Molecular Cancer . 2014,第4期

机译：激素依赖性反馈环通过限制MID1（一种新型的翻译增强剂和致癌信号的启动子）来控制雄激素受体的水平
4. Pilot- Induced Oscillation Analysis with Actuator Rate Limiting and Feedback Control Loop [C] . R. Katayanagi AIAA Guidance, Navigation, and Control Conference;Applied Aerodynamics Conference and Exhibit;AIAA/AAS Astrodynamics Specialist Conference and Exhibit . 2004

机译：具有执行器速率限制和反馈控制回路的飞行员引起的振荡分析
5. Data-Driven H∞ Loop-Shaping Controller Design and Stability of Switched Nonlinear Feedback Systems with Average Time-Variation Rate [D] . Sung, Yu-chen. 2019

机译：数据驱动的H∞环形整形控制器设计和具有平均时间变化率的交换非线性反馈系统的稳定性
6. A hormone-dependent feedback-loop controls androgen receptor levels by limiting MID1, a novel translation enhancer and promoter of oncogenic signaling [O] . Andrea Köhler, Ümmühan Demir, Eva Kickstein, 1971

机译：激素依赖性反馈环通过限制MID1（一种新型的翻译增强剂和致癌信号的启动子）来控制雄激素受体的水平
7. A Control Allocation Technique to Recover From Pilot-Induced Oscillations (CAPIO) Due to Actuator Rate Limiting [O] . Kolmanovsky Ilya V., Yildiz Yildiray 2010

机译：由于执行器速率限制而从飞行员引起的振荡（CAPIO）中恢复的一种控制分配技术
8. Prediction of Pilot-Induced Oscillations (PIO) Due to Actuator Rate Limiting Using the Open-Loop Onset Point (OLOP) Criterion [R] . Gilbreath, G. P. 2001

机译：使用开环起始点（OLOp）准则预测由于执行器速率限制导致的先导振荡（pIO）

Pilot-Induced Oscillation Analysis with Actuator Rate Limiting and Feedback Control Loop

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