首页> 外文期刊>Optimal Control Applications and Methods >Guidance and control laws design for a switched system with discontinuous actuators
【24h】

Guidance and control laws design for a switched system with discontinuous actuators

机译:具有不连续执行器的交换系统的指导和控制法设计

获取原文
获取原文并翻译 | 示例
           

摘要

Guidance and control laws design for a switched flight system with discontinuous actuators is dealt with in this paper. Firstly, a missile equipped with discontinuous side jets is introduced. Secondly, the side-jet missile is modeled with an impulsive switched system. Thirdly, a sliding mode control-based discontinuous guidance law is proposed to generate guidance commands, which are suitable for on-off side jets. And a logic-based switching law for turning on the side jets is also submitted. Fourthly, by transforming the discontinuous actuators equivalently and formulating an extended state space equation, a tracking control law is indicated to track the guidance command. Finally, simulations and comparisons are made to demonstrate the proposed algorithms. Copyright (c) 2016 John Wiley & Sons, Ltd.
机译:本文处理了具有不连续执行器的交换机系统的指导和控制法设计。 首先,介绍配备有不连续侧喷射器的导弹。 其次,侧喷射导弹采用脉冲切换系统建模。 第三,提出了一种基于滑模控制的不连续的指导法,以生成引导命令,其适用于开关侧喷射器。 还提交了一种用于打开侧喷射机的基于逻辑的交换法。 第四,通过等效地改变不连续的致动器并配制延长的状态空间方程,表示跟踪控制定律以跟踪引导命令。 最后,进行模拟和比较来展示所提出的算法。 版权所有(c)2016 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