A PHASE COMPENSATION METHOD FOR PREVENTION OF PILOT-INDUCED OSCILLATIONS DUE TO ACTUATOR RATE SATURATION

机译：一种用于防止因执行器转速饱和而引起的飞行员振动的相位补偿方法

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This paper presents a simple and effective solution for type 2 pilot-induced oscillations due to the rate limit of the control surface. The proposed method uses a nonlinear filter that compensates the phase in the control signal before feeding the actuator. The structure of this filter has advantages over previous realizations that allow tuning simplicity considering limit cycle prevention as control specification. Simulation results demonstrate the good performance of the proposed compensation.

机译：由于控制面的速率限制，本文提出了一种简单有效的解决方案，用于解决2型导频引起的振荡。所提出的方法使用非线性滤波器，该非线性滤波器在馈入致动器之前补偿控制信号中的相位。与以前的实现相比，该滤波器的结构具有很多优点，这些实现允许将极限周期预防作为控制规范，从而简化调试。仿真结果证明了所提出补偿的良好性能。

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来源
《Saint Petersburg International Conference on Integrated Navigation Systems; 20030526-28; St.Petersburg(RU)》|2003年|P.49-50|共2页
会议地点 St.Petersburg(RU)
作者
I. Alcala; J. Aracil; F. Gordillo;
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作者单位

Dpto. Ingenieria de Sistemas y Automatica, Univ. of Seville, Spain. Av. de los Descubrimientos s, 41092, Seville, Spain;

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会议组织
原文格式 PDF
正文语种 eng
中图分类导航设备;
关键词
pilot-induced oscillations (PIO); fly-by-wire (FBW); rate limiter; phase compensators;

机译：先导感应振荡（PIO）;电传飞行（FBW）;速率限制器;相位补偿器;

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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. Pilot-Induced Oscillation Analysis with Actuator Rate Limiting and Feedback Control Loop [J] . Ryoji Katayanagi 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环的飞行员感应振荡分析
3. Fixed-order dynamic compensation for linear systems with actuator amplitude and rate saturation constraints [J] . Vijay Sekhar, Chellaboina, Wassim M. Haddad, International Journal of Control . 2000,第12期

机译：具有执行器振幅和速率饱和约束的线性系统的定阶动态补偿
4. A PHASE COMPENSATION METHOD FOR PREVENTION OF PILOT-INDUCED OSCILLATIONS DUE TO ACTUATOR RATE SATURATION [C] . I. Alcala, J. Aracil, F. Gordillo Saint Petersburg International Conference on Integrated Navigation Systems . 2003

机译：由于执行器速率饱和而预防导频振荡的相位补偿方法
5. Compensation and Control Allocation with Input Saturation Limits and Rotor Faults for Multi-Rotor Copters with Redundant Actuations [D] . Su, Yao. 2021

机译：具有冗余致动的多转子矫正器的输入饱和限制和转子故障的补偿和控制分配
6. PNAS Plus: Robust efficiency and actuator saturation explain healthy heart rate control and variability [O] . Na Li, Jerry Cruz, Chenghao Simon Chien, 2014

机译：PNAS Plus：稳定的效率和执行器饱和度可解释健康的心率控制和变异性
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. Comparison of Nonlinear Algorithms in the Prevention of Pilot-Induced Oscillations Caused by Actuator Rate Limiting (Project HAVE PREVENT) [R] . Hanley, J. , Ritter, S. , Gloystein, J. , 2002

机译：非线性算法在防止执行器速率限制引起的先导振荡中的比较（项目已预防）

A PHASE COMPENSATION METHOD FOR PREVENTION OF PILOT-INDUCED OSCILLATIONS DUE TO ACTUATOR RATE SATURATION

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