Impact Angle Control Guidance Synthesis for Evasive Maneuver against Intercept Missile
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The Korean Society for Aeronautical & Space Sciences
Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Reinforcement Learning for the Interception of Hypersonic Vehicles;AIAA SCITECH 2024 Forum;2024-01-04
2. Design of Safe Optimal Guidance With Obstacle Avoidance Using Control Barrier Function-Based Actor–Critic Reinforcement Learning;IEEE Transactions on Systems, Man, and Cybernetics: Systems;2023-11
3. A hierarchical reinforcement learning method for missile evasion and guidance;Scientific Reports;2022-11-07
4. Legendre Pseudo-Spectral Method for Missile Trajectory Optimization with Free Final Time;Lecture Notes in Electrical Engineering;2022-09-30
5. L1 Penalized Sequential Convex Programming for Fast Trajectory Optimization: With Application to Optimal Missile Guidance;International Journal of Aeronautical and Space Sciences;2019-11-21
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