An Adaptive Terminal Guidance Law Based on Deep Reinforcement Learning
摘要
In order to attack maneuvering targets, high gains (i.e. navigation gain) are required in the proportional navigation guidance (PNG) laws, by which the commands of overload change fast. Since the response delay of the autopilot cannot be ignored, it is difficult for the missile to track such a fast-varying command accurately with traditional guidance law. A deep reinforcement learning-based solution for PNG is proposed, by which the trade-off issue associated with the high-gain guidance law is addressed. In this solution, the guidance gain is adjusted adaptively according to the pre-trained policy network. By applying the solution to a simulation case with head-on target, the validity of the proposed guidance law is proved.