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Attitude/Orbit Engine Compound Control for Hypersonic Target Interceptor With Discrete-Time Inputs and State Constraints.
Qian Peng
Gang Chen
Jianguo Guo
Zongyi Guo
Published in:
IEEE Trans. Aerosp. Electron. Syst. (2024)
Keyphrases
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air fuel ratio
attitudes toward
adaptive control
linear constraints
feedback control