Optimal Fault-Tolerant Control of Reusable Launch Vehicle With Actuator Faults Using Zero-Sum Differential Game Theory

Author:

Ren Hao,Ma Yajie,Jiang Bin

Publisher

Elsevier BV

Reference34 articles.

1. Attitude controller design for reusable launch vehicle during reentry phase via compound adaptive fuzzy H-infinity control;Q Mao;Aerosp. Sci. Technol,2018

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3. The design of fixed-time observer and finitetime fault-tolerant control for hy-personic gliding vehicles;X Yu;IEEE Trans. Ind. Electron,2017

4. A review on fault-tolerant cooperative control of multiple unmanned aerial vehicles;Z Q Yu;Chin. J. Aeronaut,2022

5. Fault-tolerant control and vibration suppression of flexible spacecraft: An interconnected system approach;Q Li;Chin. J. Aeronaut,2022

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