Optimal control design for two degree of freedom helicopter

机译：二自由度直升机的最优控制设计

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摘要

This paper deals with the optimal control strategy for flight control of two degree of freedom helicopter (DOF). The design is composed of various controllers for controlling pitch and yaw motions of helicopter. PID, state feedback control (SFC) and Linear Quadratic Regulator (LQR) control are designed and compared the performance of each controller with simulation results.

机译：本文研究了两自由度直升机（DOF）飞行控制的最优控制策略。该设计由各种控制器组成，用于控制直升机的俯仰和偏航运动。设计PID，状态反馈控制（SFC）和线性二次调节器（LQR）控制，并将每个控制器的性能与仿真结果进行比较。

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来源
《2015 International Conference on Energy Systems and Applications》|2015年|470-474|共5页
会议地点 Pune(IN)
作者
Santosh Nagre; C. B. Kadu; B. J. Parvat;
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作者单位

Department of Instrumentation and Control, Pravara Rural Engineering College, India;

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会议组织
原文格式 PDF
正文语种 eng
中图分类
关键词
LQR; optimal control; two DOF helicopter;

机译：LQR；最优控制；两自由度直升机;

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专利

1. Control Design by Extended Linearisation Techniques for a Two Degrees of Freedom Helicopter [J] . Saif S. Butt, Hao Sun, Harald Aschemann IFAC PapersOnLine . 2015,第11期

机译：两自由度直升机的扩展线性化技术控制设计
2. Control Design by Extended Linearisation Techniques for a Two Degrees of Freedom Helicopter [J] . Saif S. Butt, Hao Sun, Harald Aschemann IFAC PapersOnLine . 2015,第11期

机译：两自由度直升机的扩展线性化技术控制设计
3. Sampled-data-based adaptive optimal output-feedback control of a 2-degree-of-freedom helicopter [J] . Weinan Gao, Mengzhe Huang, Zhong-Ping Jiang, Control Theory & Applications, IET . 2016,第12期

机译：2自由度直升机的基于采样数据的自适应最优输出反馈控制
4. Optimal control design for two degree of freedom helicopter [C] . Santosh Nagre, C. B. Kadu, B. J. Parvat International Conference on Energy Systems and Applications . 2015

机译：两级自由直升机的最优控制设计
5. A 6-degree-of-freedom testbed for small model helicopters control evaluation. [D] . Zhao, Jun. 2008

机译：用于小型直升机控制评估的6自由度试验台。
6. Optimal Control Predicts Human Performance on Objects with Internal Degrees of Freedom [O] . Arne J. Nagengast, Daniel A. Braun, Daniel M. Wolpert 2009

机译：最佳控制可预测具有内部自由度的对象的人类性能
7. Adaptive attitude tracking control of a 3-degrees-of-freedom experimental helicopter with actuator dead-zone [O] . Chuang Li, Xuebo Yang, Bing Xiao 2018

机译：三维自由度实验直升机与执行器死区的自适应姿态跟踪控制
8. Optimal Control Design Advantages Utilizing Two-Degree-of-Freedom Controllers [R] . Stephens, M. J. 1993

机译：利用两自由度控制器的最优控制设计优势

Optimal control design for two degree of freedom helicopter

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