首页> 外文会议>Israel annual conference on aerospace sciences >UPPER BOUNDS OF MISSILE CONTROL BASED ON LINEAR-QUADRATIC DIFFERENTIAL GAME
【24h】

UPPER BOUNDS OF MISSILE CONTROL BASED ON LINEAR-QUADRATIC DIFFERENTIAL GAME

机译:基于线性二次差分游戏的导弹控制的上限

获取原文

摘要

Di erential game formulations provide an adequate basis for guidance law synthesis against highly maneuvering targets. This paper deals with a guidance law based on a linear-quadratic di erential game formulation. This guidance law has many attractive properties: it is continuous, linear by the state variables, its gain coe?cients can be precalculated o -line, etc. Nevertheless, due to the lack of "hard" control constraints in the formulation, the magnitude of the control can exceed the admissible level imposed by the nature of the problem. In this paper estimates of the interceptor's control upper bound are obtained depending on the system parameters and the penalty coe?cients of the game index. It is shown that having a su?cient maneuverability advantage and choosing properly the penalty coe?cients, the interceptor can guarantee an arbitrary small miss distance without exceeding the natural control constraints. By manipulat- ing both penalty coe?cients it is possible to reduce signi cantly the maneuverability requirements compared to the limit case of zero interceptor's penalty coe?cient.
机译:DI剥脱游戏制剂提供了对高机动目标的指导法合成的充分基础。本文涉及基于线性二次迪剥夺游戏制定的指导法。本指导法具有许多有吸引力的特性:它是连续的,线性的状态变量,它的增益COE?连续性可以预先计算Online等。然而,由于制定中缺乏“硬”控制约束,因此幅度控制可以超过问题的性质所赋予的可允许水平。在本文中,取决于系统参数和游戏索引的惩罚COE,获得了拦截器控制上限的估计。结果表明,具有苏·何种机动性优势和选择罚款COE?尼斯,拦截器可以保证任意小错过距离而不超过自然控制约束。通过操纵惩罚COE?与零拦截COE的极限情况相比,可以通过零拦截器的极限情况来降低机动性要求。

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