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Research on Helicopter Stabilator Control System

机译:直升机稳定器控制系统研究

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to deal with the problems caused by the fixed stabilator, the movable stabilator and its installation angle control system have been researched in this paper. Base on the analysis of the influence of movable stabilator on helicopter longitudinal flying qualities, the control structure of the installation angle control system has been designed and its parameters are figured out with SQP method. The control system raised in this paper could be useful to instruct the movable stabilator installation angle control system design.
机译:为了处理由固定稳定器引起的问题,本文研究了可移动稳定器及其安装角度控制系统。基于分析可移动稳定器对直升机纵向速度速度的影响,设计了安装角度控制系统的控制结构及其参数用SQP方法计算出。本文提出的控制系统可用于指示可移动稳定器安装角度控制系统设计。

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