首页> 外文期刊>Optimal Control Applications and Methods >Dynamic surface control based on neural network for an air-breathing hypersonic vehicle
【24h】

Dynamic surface control based on neural network for an air-breathing hypersonic vehicle

机译:基于神经网络的空气超音速飞行器动态表面控制

获取原文
获取原文并翻译 | 示例
           

摘要

In this paper, an adaptive dynamic surface control approach is presented for the longitudinal motion of an air-breathing hypersonic vehicle. Fully tuned radial basis function neural network that regulates weights, width, and center of Gaussian function simultaneously is developed to estimate aerodynamic uncertainties and atmospheric disturbances. The nonlinear control law is subsequently designed by dynamic surface control approach for the vehicle model converted into strict block feedback form by input-output linearization method. Simulation results show that the velocity can be successfully tracked over a large range from Mach 11 to Mach 12 and an altitude range from 26 to 30 km. The presented approach has perfect ability of restraining unknown and time-varying nonlinear dynamics during flight. Copyright (C) 2014 John Wiley & Sons, Ltd.
机译:在本文中,提出了一种用于呼吸超音速飞行器纵向运动的自适应动态表面控制方法。开发了可同时调节权重,宽度和高斯函数中心的全调谐径向基函数神经网络,以估计空气动力学的不确定性和大气干扰。随后通过动态表面控制方法设计了非线性控制律,将车辆模型通过输入输出线性化方法转换为严格的块反馈形式。仿真结果表明,可以在11马赫至12马赫的大范围内以及26至30 km的高度范围内成功跟踪速度。提出的方法具有抑制飞行过程中未知且时变的非线性动力学的完美能力。版权所有(C)2014 John Wiley&Sons,Ltd.

著录项

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