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Index Approach Law Based Sliding Control for a Hypersonic Aircraft

机译：基于索引方法定律的高超音速飞机滑行控制

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来源
《U.S. Air Force Tamp;E Days 2009》|2009年|P.1-10|共10页
会议地点 Albuquerque NM(US)
作者
L. Huifeng; S. Wenchong; L. Zhaoying; X. Song;
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作者单位

-bai, Beihang University, Beijing, China (prc);

-bai, Beihang University, Beijing, China (prc);

-bai, Beihang University, Beijing, China (prc);

-bai, Beihang University, Beijing, China (prc);

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原文格式 PDF
正文语种
中图分类空军;
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入库时间 2022-08-26 14:22:20

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1. Robust Controller of Hypersonic Aircraft Based on Grey Prediction Sliding Mode Control [J] . Jiao Xin, Jiang Ju, Xu Haiyan, The Journal of grey system . 2016,第3期

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2. Sliding mode controller design based on reaching law for hypersonic flight vehicle [J] . Jianmin Wang, Yunjie Wu, Xiaodong Liu International journal of modeling, simulation and scientific computing . 2014,第4期

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3. Adaptive attitude tracking control for hypersonic reentry vehicles via sliding mode-based coupling effect-triggered approach [J] . Guo Zongyi, Guo Jianguo, Zhou Jun Aerospace science and technology . 2018,第JULa期

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4. Index Approach Law Based Sliding Control for a Hypersonic Aircraft [C] . U.S. Air Force TE Days . 2009

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5. A Model-Free Control Algorithm Based on the Sliding Mode Control Method with Applications to Unmanned Aircraft Systems [D] . Kadungoth Sreeraj, Adarsh Raj. 2019

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6. Terminal Sliding Mode Control with a Novel Reaching Law and Sliding Mode Disturbance Observer for Inertial Stabilization Imaging Sensor [O] . Xin Che, Dapeng Tian, Ping Jia, 2020

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7. Robust Nonlinear Control of a Hypersonic Aircraft Based on Sliding Mode Control [O] . Zhubing Hu, bo Mo, Dezhi Zhou, 2012

机译：基于滑模控制的高超音速飞机鲁棒非线性控制

Index Approach Law Based Sliding Control for a Hypersonic Aircraft

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