【24h】

Recurrent-Functional-Link-Network-Based Predictive Control for Hypersonic Vehicles with Dynamical Uncertainties

机译:具有动态不确定性的超音速飞行器的基于递归功能链接网络的预测控制

获取原文

摘要

This paper presents a novel adaptive predictive control methodology for air-breathing hypersonic vehicles (AHVs) in the presence of dynamical thrust and parameter uncertainties. The method combines the nonlinear generalized predictive control (NGPC) with a new recurrent-functional-link- network (RFLN) adaptive law proposed here. The RFLN is a simple recurrent neural network without hidden layers, so it is suitable for the approximation of dynamical uncertainties during the hypersonic flight. The RFLN weights are online tuned by the derived adaptive laws based on Lyapunov stability theorem for the first time. The learning process does not need any offline training phase. Additionally, a robust controller whose gain can be adaptively adjusted is designed to recover the residual of the approximation error. Finally, simulation results show better performance of the controller for the AHV attitude tracking than the method compared, moreover, the robustness to dynamical parameters variations and the disturbance rejection are successfully accomplished.
机译:本文介绍了在存在动态推力和参数不确定性的情况下,用于呼吸超音速飞行器(AHV)的新型自适应预测控制方法。该方法将非线性广义预测控制(NGPC)与此处提出的新的递归功能链接网络(RFLN)自适应定律相结合。 RFLN是一个简单的递归神经网络,没有隐藏层,因此适用于高超声速飞行过程中动力学不确定性的近似估计。首次基于Lyapunov稳定性定理,通过导出的自适应定律对RFLN权重进行在线调整。学习过程不需要任何离线培训阶段。另外,其增益可以自适应调整的鲁棒控制器被设计为恢复近似误差的残差。最后,仿真结果表明,该控制器用于AHV姿态跟踪的性能优于所比较的方法,此外,还成功实现了对动态参数变化的鲁棒性和干扰抑制。

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号