Output feedback fault-tolerant control for hypersonic flight vehicles with non-affine actuator faults-Reference-Cited by-同舟云学术

Output feedback fault-tolerant control for hypersonic flight vehicles with non-affine actuator faults

Published:2022-04 Issue: Volume:193 Page:324-337
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Lu Yao^ORCID,Jia Zhiqiang,Liu Xiaodong,Lu Kunfeng

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference37 articles.

1. Analytical solutions to three-dimensional hypersonic gliding trajectory over rotating Earth;Zhang;Acta Astronaut.,2021

2. 3D guidance for hypersonic reentry gliders based on analytical prediction;Pan;Acta Astronaut.,2020

3. Trajectory planning for hypersonic reentry vehicle satisfying deterministic and probabilistic constraints;Chai;Acta Astronaut.,2020

4. Active disturbance rejection control based robust output feedback autopilot design for airbreathing hypersonic vehicles;Tian;ISA Trans.,2018

5. Scheduled composite off-line output feedback model predictive control for a constrained hypersonic vehicle using polyhedral invariant sets;Ma;J. Aero. Eng.,2018

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