Terminal Sliding Mode Control with Unidirectional Auxiliary Surfaces for Hypersonic Vehicles Based on Adaptive Disturbance Observer

He Naibao; Jiang Changsheng; Jiang Bin; Gao Qian

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Terminal Sliding Mode Control with Unidirectional Auxiliary Surfaces for Hypersonic Vehicles Based on Adaptive Disturbance Observer

机译：基于自适应扰动观测器的超音速飞行器单向辅助表面终端滑模控制

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A novel flight control scheme is proposed using the terminal sliding mode technique, unidirectional auxiliary surfaces and the disturbance observer model. These proposed dynamic attitude control systems can improve control performance of hypersonic vehicles despite uncertainties and external disturbances. The terminal attractor is employed to improve the convergence rate associated with the critical damping characteristics problem noted in short-period motions of hypersonic vehicles. The proposed robust attitude control scheme uses a dynamic terminal sliding mode with unidirectional auxiliary surfaces. The nonlinear disturbance observer is designed to estimate system uncertainties and external disturbances. The output of the disturbance observer aids the robust adaptive control scheme and improves robust attitude control performance. Finally, simulation results are presented to illustrate the effectiveness of the proposed terminal sliding mode with unidirectional auxiliary surfaces.

机译：利用终端滑模技术，单向辅助表面和扰动观测器模型，提出了一种新颖的飞行控制方案。尽管存在不确定性和外部干扰，但是这些提出的动态姿态控制系统可以改善高超声速车辆的控制性能。终端吸引子用于提高与高超声速飞行器短周期运动中注意到的临界阻尼特性问题相关的收敛速度。所提出的鲁棒姿态控制方案使用具有单向辅助表面的动态终端滑模。非线性干扰观测器旨在估计系统不确定性和外部干扰。干扰观测器的输出有助于鲁棒的自适应控制方案并提高鲁棒的姿态控制性能。最后，仿真结果表明了所提出的具有单向辅助表面的终端滑模的有效性。

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《Mathematical Problems in Engineering》 |2015年第16期|285716.1-285716.11|共11页
作者
He Naibao; Jiang Changsheng; Jiang Bin; Gao Qian;
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Jiangsu Univ Technol, Sch Elect & Informat Engn, Changzhou 213001, Peoples R China.;

Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 210016, Peoples R China.;

Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 210016, Peoples R China.;

Jiangsu Univ Technol, Sch Comp Engn, Changzhou 213001, Peoples R China.;

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1. Adaptive neural network disturbance observer based nonsingular fast terminal sliding mode control for a constrained flexible air-breathing hypersonic vehicle [J] . Ma Yu, Cai Yuanli, Yu Zhenhua Proceedings of the Institution of Mechanical Engineers . 2019,第7期

机译：约束柔性呼吸高超声速飞行器基于自适应神经网络扰动观测器的非奇异快速终端滑模控制
2. Adaptive neural network disturbance observer based nonsingular fast terminal sliding mode control for a constrained flexible air-breathing hypersonic vehicle [J] . Ma Yu, Cai Yuanli, Yu Zhenhua Proceedings of the Institution of Mechanical Engineers . 2019,第7期

机译：基于自适应神经网络扰动观测器的受限柔性空气呼吸超声波的非垂直终端滑动模式控制
3. Adaptive terminal sliding mode control for hypersonic flight vehicles with strictly lower convex function based nonlinear disturbance observer [J] . Wu Yun-jie, Zuo Jing-xing, Sun Liang-hua ISA Transactions . 2017,第Pta2期

机译：具有严格下凸函数基于非线性扰动观测器的高效飞行车辆自适应终端滑模控制
4. Sliding Mode Control with Unidirectional Auxiliary Surfaces Based on Double Power Reaching Law and Disturbance Observer [C] . Wutong Xu, Long Qiu, Dian Sheng, Chinese Control Conference . 2017

机译：基于双功率达到法律和干扰观测器的单向辅助表面滑动模式控制
5. Hyper sonic missile control in terminal mode using continuous higher order sliding mode control driven by disturbance observer. [D] . Yu, Polk. 2013

机译：使用由扰动观测器驱动的连续高阶滑模控制，以终端模式控制超音速导弹。
6. Synchronization of a Non-Equilibrium Four-Dimensional Chaotic System Using a Disturbance-Observer-Based Adaptive Terminal Sliding Mode Control Method [O] . Shaojie Wang, Amin Yousefpour, Abdullahi Yusuf, 2020

机译：使用干扰观察者的自适应终端滑动模式控制方法同步非平衡四维混沌系统
7. Terminal Sliding Mode Control with Unidirectional Auxiliary Surfaces for Hypersonic Vehicles Based on Adaptive Disturbance Observer [O] . Naibao He, Changsheng Jiang, Bin Jiang, 2015

机译：基于自适应干扰观测器的超音速车辆具有单向辅助表面的终端滑模控制

Terminal Sliding Mode Control with Unidirectional Auxiliary Surfaces for Hypersonic Vehicles Based on Adaptive Disturbance Observer

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