Design method of an intelligent pilot for missiles under space constraint
Author:
Affiliation:
1. Nanjing University of Science and Technology,Nanjing,China
2. Nanjing University of Science and Technology, Ministry of Education,Key Laboratory of Maritime Intelligent Cyberspace Technology,Nanjing,China
Funder
National Natural Science Foundation of China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10280771/10280779/10281137.pdf?arnumber=10281137
Reference15 articles.
1. Optimal Intelligent Control for Doubly Fed Induction Generators
2. Deep deterministic policy gradient algorithm for unmanned aerial vehicle control[J];huang;Journal of Aeronautics,2021
3. Deep reinforcement learning method for turbofan engine acceleration optimization problem within full flight envelope
4. Parameter design of launch vehicle attitude controller based on DDQN[J];huang;Control of Spacecraft,2020
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