| 鱼雷静不稳定状态下纵向三回路过载控制与仿真研究 |
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| 引用本文： | 李世雄. 鱼雷静不稳定状态下纵向三回路过载控制与仿真研究[J]. 适用技术之窗, 2010, 0(9): 6-9 |
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| 作者姓名： | 李世雄 |
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| 作者单位： | 海军驻昆明地区军事代表室,云南昆明650000 |
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| 摘 要： | 静不稳定控制技术作为现代航空航天、水中兵器主动控制技术,在近些年逐渐成为研究热点。本文针对某静不稳定鱼雷,建立了纵向运动模型,运用最优控制理论设计了俯仰通道三回路过载控制系统,最后对设计出的控制器进行了特征点控制系统仿真。结果说明,三回路过载控制方法能较好地控制静不稳定鱼雷。
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| 关 键 词： | 静不稳定 最优控制理论 三回路过载控制 仿真 |
Research on Longitudinal Control of Unstable Missle Using Three Loop Acceleration and Simulation |
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| Li Shixiong. Research on Longitudinal Control of Unstable Missle Using Three Loop Acceleration and Simulation[J]. Science & Technology Plaza, 2010, 0(9): 6-9 |
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| Authors: | Li Shixiong |
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| Affiliation: | Li Shixiong(Navy＇s Military Representive Office in Kunming,Yunnan Kunming 650000) |
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| Abstract: | Unstable missile control technology is a modern active control technology.It becomes a research point in recent years.We establish a missile longitudinal model use an unstable missile and design the three loop acceleration control on longitudinal based on the theory of optimal control.Then we simulate the control system that we designed at the characteristic flying point,and the result show that the three loop acceleration control can control the unstable missile quite well. |
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| Keywords: | Static Unstable Missile Optimal Control theory Three Loop Acceleration Control Simulation |
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