首页 | 本学科首页   官方微博 | 高级检索  
     检索      

Model-free adaptive optimal design for trajectory tracking control of rocket-powered vehicle
作者姓名:Wenming NIE  Huifeng LI  Ran ZHANG
作者单位:1. School of Astronautics, Beihang University;2. Key Laboratory of Spacecraft Design Optimization and Dynamic Simulation Technologies, Ministry of Education
摘    要:An adaptive optimal trajectory tracking controller is presented for the Solid-RocketPowered Vehicle(SRPV) with uncertain nonlinear non-affine dynamics in the framework of adaptive dynamic programming. First, considering that the ascent model of the SRPV is non-affine, a model-free Single Network Adaptive Critic(SNAC) method is developed based on the dynamic neural network and the traditional SNAC method. This developed model-free SNAC method overcomes the limitation of the traditional SNAC metho...

收稿时间:15 May 2019

Model-free adaptive optimal design for trajectory tracking control of rocket-powered vehicle
Wenming NIE,Huifeng LI,Ran ZHANG.Model-free adaptive optimal design for trajectory tracking control of rocket-powered vehicle[J].Chinese Journal of Aeronautics,2020,33(6):1703-1716.
Institution:1. School of Astronautics, Beihang University, Beijing 100083, China;2. Key Laboratory of Spacecraft Design Optimization and Dynamic Simulation Technologies, Ministry of Education, Beijing 100083, China
Abstract:An adaptive optimal trajectory tracking controller is presented for the Solid-Rocket-Powered Vehicle (SRPV) with uncertain nonlinear non-affine dynamics in the framework of adaptive dynamic programming. First, considering that the ascent model of the SRPV is non-affine, a model-free Single Network Adaptive Critic (SNAC) method is developed based on the dynamic neural network and the traditional SNAC method. This developed model-free SNAC method overcomes the limitation of the traditional SNAC method that can only be applied to affine systems. Then, a closed-form adaptive optimal controller is designed for the non-affine dynamics of SRPVs. This controller can adjust its parameters under different flight conditions and converge to the approximate optimal controller through online self-learning. Finally, the convergence to the approximate optimal controller is proved. The theoretical analysis of the uniformly ultimate boundedness of the tracking error is also presented. Simulation results demonstrate the effectiveness of the proposed controller.
Keywords:Adaptive dynamic programming  Dynamic neural network  Model-free  Solid-rocket-powered vehicle  Trajectory tracking
本文献已被 ScienceDirect 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号