| 飞机横侧向CAS控制律解耦设计 |
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| 引用本文： | 张翔伦,李志信.飞机横侧向CAS控制律解耦设计[J].飞行力学,1995,13(4):39-46. |
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| 作者姓名： | 张翔伦 李志信 |
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| 摘 要： | 为了解决飞机横侧向运动间的相互耦合给飞机操纵和控制系统的设计带来的诸多的不便，提出一种解耦设计方案，使得横侧系统分为两个相互独立的子系统，简化了问题的分析，比较圆满完成了飞机横侧向控制增稳系统的控制律设计，改善了飞机的操纵稳定特性。
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| 关 键 词： | 控制增稳系统 解耦 滚转轴 飞机 |
UNCOUPLED DESIGN OF AIRCRAFT LATERAL CAS CONTROL LAW |
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| Zhang Xianglun,Li Zhixin.UNCOUPLED DESIGN OF AIRCRAFT LATERAL CAS CONTROL LAW[J].Flight Dynamics,1995,13(4):39-46. |
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| Authors: | Zhang Xianglun Li Zhixin |
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| Institution: | Flig ht Automatic Control Research Institute |
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| Abstract: | The rolling and the yawing motions of an aircraft are coupled,which putsaircraft manipulation and flight control system design to inconvenience,This paper presentsan uncoupled design scheme,which divides the lateral system into two independent subsys-tems,simplifies the problem analysis,accomplishes the control law design of aircraft lateralCAS and improves aircraft stability. |
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| Keywords: | Control Augment System(CAS)Uncouple Rolling axis Tracecharacteristic |
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