Flight and Vibration Control of Flexible Air-Breathing Hypersonic Vehicles Under Actuator Faults-Reference-Cited by-同舟云学术

Flight and Vibration Control of Flexible Air-Breathing Hypersonic Vehicles Under Actuator Faults

Published:2023-05 Issue:5 Volume:53 Page:2741-2752
ISSN:2168-2267
Container-title:IEEE Transactions on Cybernetics
language:
Short-container-title:IEEE Trans. Cybern.

Author:

He Xiuyu¹^ORCID,Ma Yonghao¹^ORCID,Chen Mou²^ORCID,He Wei¹^ORCID

Affiliation:

1. Institute of Artificial Intelligence and School of Automation and Electrical Engineering, University of Science and Technology Beijing, Beijing, China

2. College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China

Funder

National Natural Science Foundation of China

Postdoctor Research Foundation of Shunde Graduate School of University of Science and Technology Beijing

China Postdoctoral Science Foundation

Beijing Top Discipline for Artificial Intelligence Science and Engineering, University of Science and Technology Beijing

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Subject

Electrical and Electronic Engineering,Computer Science Applications,Human-Computer Interaction,Information Systems,Control and Systems Engineering,Software

Link

http://xplorestaging.ieee.org/ielx7/6221036/10106628/09732281.pdf?arnumber=9732281

Reference60 articles.

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

2. Adaptive finite-time back-stepping global sliding mode tracker of quad-rotor UAVs under model uncertainty, wind perturbation and input saturation;mofid;IEEE Trans Aerosp Electron Syst,2021

3. Robust Adaptive Fuzzy Control for HFV With Parameter Uncertainty and Unmodeled Dynamics

4. Stabilization for a Hybrid System of Elasticity with Boundary Disturbances

5. Robust adaptive neural control of flexible hypersonic flight vehicle with dead-zone input nonlinearity

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