Composite Attitude Tracking Control for Launch Vehicles Subject to Actuator Degradation Fault and Multiple Disturbances-Reference-Cited by-同舟云学术

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Composite Attitude Tracking Control for Launch Vehicles Subject to Actuator Degradation Fault and Multiple Disturbances

Published:2024-07 Issue:7 Volume:20 Page:9275-9285
ISSN:1551-3203
Container-title:IEEE Transactions on Industrial Informatics
language:
Short-container-title:IEEE Trans. Ind. Inf.

Author:

Teng Hao¹^ORCID,Zhu Yukai²^ORCID,Qiao Jianzhong¹^ORCID,Yao Xiuming³^ORCID,Guo Lei¹^ORCID

Affiliation:

1. School of Automation Science and Electrical Engineering, Beihang University, Beijing, China

2. School of Astronautics, Beihang University, Beijing, China

3. School of Electronic and Information Engineering, Beijing Jiaotong University, Beijing, China

Funder

National Natural Science Foundation of China

Beijing Natural Science Foundation

Fundamental Research Funds for the Central Universities

China Aerospace Science and Technology Corporation

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Link

http://xplorestaging.ieee.org/ielx7/9424/10582275/10500443.pdf?arnumber=10500443

Reference33 articles.

1. Entry Trajectory Optimization With Virtual Motion Camouflage Principle

2. Robust Guidance for A Reusable Launch Vehicle in Terminal Phase

3. Adaptive Multivariable Reentry Attitude Control of RLV With Prescribed Performance

4. Semi-globally smooth control for VTVL reusable launch vehicle under actuator faults and attitude constraints

5. Comprehensive design of uniform robust exact disturbance observer and fixed‐time controller for reusable launch vehicles

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1. Performance-prescribed optimal neural control for hypersonic vehicles considering disturbances: An adaptive dynamic programming approach;Aerospace Science and Technology;2024-09

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