Real-Time Optimal Approach and Capture of ENVISAT Based on Neural Networks

被引:8
作者
Li, Hongjue [1 ,2 ]
Dong, Yunfeng [1 ,2 ]
Li, Peiyun [1 ,2 ]
机构
[1] Beihang Univ, Sch Astronaut, Beijing 100191, Peoples R China
[2] Minist Educ, Key Lab Spacecraft Design Optimizat & Dynam Simul, Beijing 100191, Peoples R China
关键词
COLLISION-AVOIDANCE; PROXIMITY OPERATIONS; SPACECRAFT; GUIDANCE; ATTITUDE; TARGET;
D O I
10.1155/2020/8165147
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A neural network-based controller is developed to enable a chaser spacecraft to approach and capture a disabled Environmental Satellite (ENVISAT). This task is conventionally tackled by framing it as an optimal control problem. However, the optimization of such a problem is computationally expensive and not suitable for onboard implementation. In this work, a learning-based approach is used to rapidly generate the control outputs of the controller based on a series of training samples. These training samples are generated by solving multiple optimal control problems with successive iterations. Then, Radial Basis Function (RBF) neural networks are designed to mimic this optimal control strategy from the generated data. Compared with a traditional controller, the neural network controller is able to generate real-time high-quality control policies by simply passing the input through the feedforward neural network.
引用
收藏
页数:17
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