| 一种攻击大机动目标的变参数组合导引律 |
| |
| 引用本文： | 左斌,李静,胡云安.一种攻击大机动目标的变参数组合导引律[J].飞行力学,2007,25(2):46-49. |
| |
| 作者姓名： | 左斌 李静 胡云安 |
| |
| 作者单位： | 海军航空工程学院,控制工程系,山东,烟台,264001 |
| |
| 摘 要： | 针对目标作大机动时的导引问题,提出了一种既简单又有效的比例加变结构组合导引律,给出了其设计机理,并在理论上对变参数进行了优化设计。通过仿真结果比较,验证了此组合导引律可以在固定时间内明显地减少追踪者的脱靶量。
|
| 关 键 词： | 比例导引 变结构导引 组合导引 |
| 文章编号： | 1002-0853（2007）02-0046-04 |
| 修稿时间： | 2006-04-012006-12-24 |
A Parameter-Variable Integrated Guidance Law Against Big Maneuvering Target |
| |
| ZUO Bin,LI Jing,HU Yun-an.A Parameter-Variable Integrated Guidance Law Against Big Maneuvering Target[J].Flight Dynamics,2007,25(2):46-49. |
| |
| Authors: | ZUO Bin LI Jing HU Yun-an |
| |
| Institution: | Department of Control Engineering, NAEI, Yantai 264001, China |
| |
| Abstract: | An integrated guidance law combining the proportional navigation and variable structure guidance laws is proposed against big maneuvering target in this paper.Certainly,the structure of the integrated guidance law is simple.The designed mechanism is explained and the variable parameters are optimized.The simulation results show that the missile can effectively intercept the target in a fixed time. |
| |
| Keywords: | proportional navigation variable structure guidance integrated guidance |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
