Adaptive neuro-control for spacecraft attitude control

K. Krishnakumar, S. Rickard, Susan Bartholomew
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引用次数: 37

Abstract

The spacecraft attitude control which combines the concepts of artificial neural networks and nonlinear adaptive control, is investigated as an alternative to linear control approaches. Two capabilities of neuro-controllers are demonstrated using a nonlinear model of the Space Station Freedom. These capabilities are: 1) synthesis of robust nonlinear controllers using neural networks; and 2) adaptively modifying neuro-controller characteristics for varying inertia characteristics. The main components of the adaptive neuro-controllers include an identification network and a controller network. Both these networks are trained using the backpropagation of error learning paradigm. To ensure robustness of the neuro-controller, an optimally connected neural network is synthesized for the identification network. For the online adaptive control problem, a new technique using a memory filter for error backpropagation is introduced. The performances of the nonlinear neuro-controllers for cases listed above are verified using a nonlinear simulation of the Space Station. Results presented substantiate the feasibility of using neural networks in robust nonlinear adaptive control of spacecraft.<>
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航天器姿态控制的自适应神经控制
结合人工神经网络和非线性自适应控制的概念,研究了航天器姿态控制作为线性控制方法的替代方案。利用空间站自由度的非线性模型论证了神经控制器的两种功能。这些能力包括:1)利用神经网络合成鲁棒非线性控制器;2)自适应修改神经控制器特性以适应不同的惯性特性。自适应神经控制器的主要组成部分包括识别网络和控制器网络。这两种网络都使用错误学习范式的反向传播进行训练。为了保证神经控制器的鲁棒性,对辨识网络合成了最优连接的神经网络。针对在线自适应控制问题,提出了一种利用记忆滤波器进行误差反向传播的新方法。通过对空间站的非线性仿真,验证了上述情况下非线性神经控制器的性能。实验结果证明了神经网络在航天器鲁棒非线性自适应控制中的可行性
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