| 按降低轨迹灵敏度综合最优设计飞行控制系统 |
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| 引用本文： | 刘明俊,吴大有,马宏绪.按降低轨迹灵敏度综合最优设计飞行控制系统[J].航天控制,1992(4). |
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| 作者姓名： | 刘明俊 吴大有 马宏绪 |
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| 作者单位： | 国防科技大学自动控制系
(刘明俊，吴大有)，国防科技大学自动控制系(马宏绪) |
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| 摘 要： | 本文提出了一个按降低轨迹灵敏度综合最优设计飞行控制系统的方法。它能使系统具有满意的动态品质,同时对系统参数的变化及非线性产生的影响具有较强的鲁棒性。该设计方法具有通用性和程序化,系统实现简单。
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| 关 键 词： | 最佳控制 飞行控制系统 航迹控制 |
Synthesis of Flight Control Systems with Optimal Design Based on Reducing Trajectory Sensitivity |
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| Liu Mingjun,Wu Dayou,Ma Hongxu Defence Science and Technology University Automatic Control.Synthesis of Flight Control Systems with Optimal Design Based on Reducing Trajectory Sensitivity[J].Aerospace Control,1992(4). |
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| Authors: | Liu Mingjun Wu Dayou Ma Hongxu Defence Science and Technology University Automatic Control |
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| Institution: | Liu Mingjun;Wu Dayou;Ma Hongxu Defence Science and Technology University Automatic Control Department |
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| Abstract: | In this paper, a direct procedures for synthesis the flight control systems with optimal
design based on reducing trajectory sensitivity are presented. The procedures provide the sys-
tems a satified dynamic qualities. It also has robustness to variations of the system parameters
and non--Linear effects. The designing method has advantages of simplicity, Versatility and
programming. |
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| Keywords: | Optimal control Flight control system Flight path control |
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