| 一种用于现代战斗机的最优滑模导引律及其仿真研究 |
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| 引用本文： | 凌利,沈春林. 一种用于现代战斗机的最优滑模导引律及其仿真研究[J]. 电光与控制, 2005, 12(2): 6-10,26 |
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| 作者姓名： | 凌利 沈春林 |
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| 作者单位： | 南京航空航天大学自动化学院,江苏,南京,210016;南京航空航天大学自动化学院,江苏,南京,210016 |
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| 摘 要： | 应用变结构控制理论推导出一种基于遗传算法优化的最优滑模导引律(OSMG),克服了传统的比例导引(PNG)在攻击机动目标时能耗大、时间长的缺点。仿真结果表明:应用此导引律,导引时间短,轨迹较为平直,适用于对现代战斗机的导引控制。
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| 关 键 词： | 战斗机导引 最优导引律 滑模导引 遗传算法 |
| 文章编号： | 1671-637X(2005)02-0006-05 |
An optimal sliding-mode guidance law for modern fighters and its simulation |
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| LING li,SHEN Chun-lin. An optimal sliding-mode guidance law for modern fighters and its simulation[J]. Electronics Optics & Control, 2005, 12(2): 6-10,26 |
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| Authors: | LING li SHEN Chun-lin |
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| Abstract: | Referring to the theory of variable structure control, an Optimal Sliding-Mode Guidance (OSMG) law optimized by genetic algorithms is proposed in this paper.It overcomes the shortcomings of great power consumption and long time in maneuvering-target attacking with traditional Proportional Navigation Guidance (PNG). Simulation shows that by the use of this guidance law, the guidance time is shorter and the trajectory is more straight, so it can be applied to the guidance control of modern fighters . |
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| Keywords: | guidance of fighters optimal guidance law sliding-mode guidance genetic algorithms |
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