• 主题
高级搜索  >
历史搜索 清空历史
首页> 外文会议>ASME Dynamic Systems and Control Conference >COMPUTATIONALLY EFFICIENT NONLINEAR H{sub}∞ CONTROL DESIGNS FOR A RIGID BODY SPACECRAFT
【24h】

COMPUTATIONALLY EFFICIENT NONLINEAR H{sub}∞ CONTROL DESIGNS FOR A RIGID BODY SPACECRAFT

机译：计算上高效的非线性H {SUB} rig刚体航天器的控制设计

获取原文
页面导航
  • 摘要
  • 著录项
  • 相似文献
  • 相关主题

摘要

In this paper, we consider nonlinear control of a symmetric spacecraft about its axis of symmetry with two control torques. Using a computationally efficient H{sub}∞ control design procedure, attitude regulation and trajectory tracking problems of the axi-symmetric spacecraft were solved. Resorting to higher order Lyapunov functions, the employed nonlinear H{sub}∞ control approach reformulates the difficult Hamilton-Jacobian-Isaacs (HJI) inequalities as semi-definite optimization conditions. Sum-of-squares (SOS) programming techniques are then applied to obtain computationally tractable solutions, from which nonlinear control laws will be constructed. The proposed nonlinear H{sub}∞ designs will be able to exploit the most suitable forms of Lyapunov function for spacecraft control and the resulting controllers will perform better than existing nonlinear control laws.
机译：在本文中，我们考虑与两个控制扭矩的对称轴对称航天器的非线性控制。使用计算上高效的H {子}∞控制设计过程，解决了AXI-Commetric SpaceCraft的姿态调节和轨迹跟踪问题。借助高阶Lyapunov功能，所用的非线性H {Sub}控制方法将困难的Hamilton-jacobian-Isaacs（HJI）的不等式重新加以为半定优化条件。然后应用方块（SOS）编程技术以获得计算易解的解决方案，从而构建非线性控制法。所提出的非线性H {Sub}∞设计将能够利用最合适的Lyapunov功能，用于航天器控制，并且所产生的控制器将比现有的非线性控制法更好。

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