| 引用本文: | 张运喜,孙明玮,陈增强.滑模变结构有限时间收敛制导律[J].控制理论与应用,2012,29(11):1413~1418.[点击复制] |
| ZHANG Yun-xi,SUN Ming-wei,CHEN Zeng-qiang.Sliding-mode variable structure finite-time convergence guidance law[J].Control Theory and Technology,2012,29(11):1413~1418.[点击复制] |
|
| 滑模变结构有限时间收敛制导律 |
| Sliding-mode variable structure finite-time convergence guidance law |
| 摘要点击 3560 全文点击 2581 投稿时间：2011-10-30 修订日期：2012-04-24 |
| 查看全文 查看/发表评论 下载PDF阅读器 |
| DOI编号 10.7641/j.issn.1000-8152.2012.11.CCTA111222 |
| 2012,29(11):1413-1418 |
| 中文关键词 导弹制导 滑模控制 制导律 入射角约束 有限时间收敛 |
| 英文关键词 missile guidance sliding-mode control guidance law incident-angle constraint finite-time convergence |
| 基金项目 国家自然科学基金资助项目(61174094, 60904064); 天津市科技支撑计划资助项目(09ZCKFSF00500); 高等学校博士学科点专项科研基金资助项目(20090031110029); 新世纪优秀人才支持计划资助项目(NCET-10-0506). |
|
| 中文摘要 |
| 针对末端有入射角度约束的制导系统, 基于滑模变结构控制思想设计了一种有限时间收敛的滑模制导律, 使制导系统的视线角速率快速收敛到零, 并令弹道倾角收敛到期望的入射角度. 通过非线性控制系统的有限时间稳定性理论对该制导律进行了分析, 给出了制导系统有限收敛时间的数学形式, 证明了制导系统的有限时间收敛性. 最后通过仿真进一步验证了该制导方法的有效性和鲁棒性. |
| 英文摘要 |
| Based on the sliding-mode variable structure control, a finite-time convergent sliding-mode guidance law is presented for the guidance systems with terminal incident angle constraint. This guidance law ensures the angular rate of the line-of-sight (LOS) to converge to zero rapidly, while the missile angular converges to the desired incident angle. By employing the finite-time stability theory of nonlinear control systems to analyze the guidance law, we obtain the mathematical expression of the convergence time, thus confirming the finite-time convergence of the guidance system. Simulation results show that the guidance law is effective and robust. |