Fault-Tolerant Track Control of Hypersonic Vehicle Based on Fast Terminal Sliding Mode-Reference-Cited by-同舟云学术

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Fault-Tolerant Track Control of Hypersonic Vehicle Based on Fast Terminal Sliding Mode

Published:2017-11 Issue:6 Volume:54 Page:1304-1316
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Sun Jing-Guang¹,Song Shen-Min¹,Wu Guan-Qun¹

Affiliation:

1. Harbin Institute of Technology, 150 001 Harbin, People’s Republic of China

Funder

National Natural Science Foundation of China under Grant

foundation for Creative Research Groups of the National Natural Science Foundation under Grant

Aeronautical Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A33890

Reference30 articles.

1. Adaptive Control and the NASA X-15-3 Flight Revisited

2. An overview on flight dynamics and control approaches for hypersonic vehicles

3. Flight Dynamics and Control of Air-Breathing Hypersonic Vehicles: Review and New Directions

4. Nonlinear Longitudinal Dynamical Model of an Air-Breathing Hypersonic Vehicle

5. Fault-Tolerant Control Laws against Sensors Failures for Hypersonic Flight

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1. Automatic Attitude Control of the Launch Vehicles by means of the Backstepping Control Method;2024 International Conference on Control, Automation and Diagnosis (ICCAD);2024-05-15

2. A Finite‐Time Fractional‐Order Error Extended State Observer for Hypersonic Vehicle;International Journal of Aerospace Engineering;2024-01

3. Prescribed-Time Guidance Law with Approach Angle Constraint and Actuator Faults;Journal of Aerospace Engineering;2024-01

4. Fault-Tolerant Control for Carrier-Based Aircraft Based on Adaptive Fuzzy Sliding-Mode Method;Applied Sciences;2023-11-26

5. Adaptive fault-tolerant control for non-minimum phase hypersonic vehicles based on adaptive dynamic programming;Chinese Journal of Aeronautics;2023-11

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