Robust Optimal Controller Design for Generic Hypersonic Vehicles-Reference-Cited by-同舟云学术

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Robust Optimal Controller Design for Generic Hypersonic Vehicles

Published:2017-07 Issue:4 Volume:30 Page:04017016
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Liu Hao¹,Liu Deyuan²,Yu Yao³

Affiliation:

1. Lecturer, School of Astronautics, Beihang Univ., Beijing 100191, P.R. China (corresponding author).

2. Ph.D. Student, School of Astronautics, Beihang Univ., Beijing 100191, P.R. China.

3. Associate Professor, School of Automation and Electrical Engineering, Univ. of Science and Technology Beijing, Beijing 100083, P.R. China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000722

Reference24 articles.

1. Non-linear control of an uncertain hypersonic aircraft model using robust sum-of-squares method

2. Uncertainty Modeling and Fixed-Order Controller Design for a Hypersonic Vehicle Model

3. Nonlinear Robust Adaptive Control of Flexible Air-Breathing Hypersonic Vehicles

4. Fuzzy guaranteed cost tracking control for a flexible air-breathing hypersonic vehicle

5. Guaranteed cost control with poles assignment for a flexible air-breathing hypersonic vehicle

Cited by 6 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Adaptive Terminal Sliding Mode Control for Flexible Air-Breathing Hypersonic Vehicle;AIAA Scitech 2021 Forum;2021-01-04

2. Parameter Adaptive Terminal Sliding Mode Control of Flexible Coupling Air-Breathing Hypersonic Vehicle;International Journal of Aerospace Engineering;2020-07-11

3. Parameter Adaptive Terminal Sliding Mode Control of Flexible Coupling Air-Breathing Hypersonic Vehicle;AIAA Scitech 2020 Forum;2020-01-05

4. Active disturbance rejection control based robust output feedback autopilot design for airbreathing hypersonic vehicles;ISA Transactions;2018-03

5. A probabilistic robust mixed H2/H∞ fuzzy control method for hypersonic vehicles based on reliability theory;International Journal of Advanced Robotic Systems;2018-01-01

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