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Attitude/Orbit Engine Compound Control for Hypersonic Target Interceptor With Discrete-Time Inputs and State Constraints
IEEE Transactions on Aerospace and Electronic Systems ( IF 4.4 ) Pub Date : 2024-04-09 , DOI: 10.1109/taes.2024.3384929 Qian Peng 1 , Gang Chen 1 , Jianguo Guo 2 , Zongyi Guo 2
中文翻译:
具有离散时间输入和状态约束的高超声速目标拦截器姿态/轨道发动机复合控制
更新日期:2024-04-09
IEEE Transactions on Aerospace and Electronic Systems ( IF 4.4 ) Pub Date : 2024-04-09 , DOI: 10.1109/taes.2024.3384929 Qian Peng 1 , Gang Chen 1 , Jianguo Guo 2 , Zongyi Guo 2
Affiliation
中文翻译:
具有离散时间输入和状态约束的高超声速目标拦截器姿态/轨道发动机复合控制