Improving Conventional Longitudinal Missile Autopilot Using Cerebellar Model Articulation Controller Neural Networks

C. C. Lin*, Fu-Chuang Chen

*此作品的通信作者

研究成果: Article同行評審

11 引文 斯高帕斯(Scopus)

摘要

A way to integrate the cerebellar model articulation controller (CMAC) neural network with the missile longitudinal conventional feedback controller (CFC) to compensate for nonlinearities, unmodeled dynamics, parameter variations, etc., is proposed. The inner loop of the CFC will essentially be left unchanged to improve the stability of the missile. The outer loop of CFC, in addition to playing its traditional role, would work with the CMAC to learn quickly to approximate the dynamic inversion from angle of attack to control deflection, to achieve better tracking in normal acceleration. In this arrangement, the well-known CFC acts as a safety net, whereas additional performance is brought about through CMAC learning.

原文American English
頁(從 - 到)711-718
頁數8
期刊Journal of Guidance, Control, and Dynamics
26
發行號5
DOIs
出版狀態Published - 1 1月 2003

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