Attitude/Orbit Engine Compound Control for Hypersonic Target Interceptor With Discrete-Time Inputs and State ConstraintsQian Peng,Gang Chen,Jianguo Guo,Zongyi GuoIEEE Transactions on Aerospace and Electronic Systems（2024）引用 0|浏览4暂无评分AI 理解论文溯源树样例生成溯源树，研究论文发展脉络Chat Paper正在生成论文摘要
