首页> 外文会议>Congress of the International Council of the Aeronautical Sciences;ICAS 2010 >DYNAMIC MODELING AND CONTROL SYSTEM FOR A SHROUDED PROPELLER SYSTEM
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DYNAMIC MODELING AND CONTROL SYSTEM FOR A SHROUDED PROPELLER SYSTEM

机译:螺旋桨推进系统动态建模与控制系统。

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This paper is presents the dynamic modelingrnand control system design of a shroudedrnpropeller based on the classical method. Therndynamic model has been designed usingrnnonlinear aerodynamic models by VLM (VortexrnLattex Method). The aerodynamic analysis ofrnthe model is indispensible for the improvementrnof its accuracy and for designing the controller.rnBased on the LTI model of hover, classicalrnSISO control has been used for the stabilizationrnof the vehicle. The controller for hover has beenrndesigned using the linear SISO control approach.rnFurther, the control system design has beenrnbased on the precise dynamic model for morernaccurate controller gain selection. The proposedrncontrollers have been presented along with thernsimulation results. In conclusion, thernperformance of the proposed approach has firstrnbeen validated by numerical simulation and thenrnby a series of flight tests.
机译:本文提出了一种基于经典方法的带罩螺旋桨动态建模与控制系统设计。通过VLM(VortexrnLattex方法)使用非线性空气动力学模型设计了动力学模型。该模型的空气动力学分析对于提高其精度和设计控制器是必不可少的。基于悬停的LTI模型,经典的SISO控制已用于车辆的稳定化。悬停控制器采用线性SISO控制方法进行了设计。此外,控制系统设计基于精确的动态模型进行了更精确的控制器增益选择。提出了控制器,并给出了仿真结果。总之,首先通过数值模拟验证了所提方法的性能,然后通过一系列飞行测试。

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