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Flight Control Experiment of Multipurpose-Aviation-Laboratory-alpha In-Flight Simulator

机译:多功能航空实验室α飞行器模拟器的飞行控制实验

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This paper reports the results of experimental verification of flight controllers for the multipurpose-aviation-rnlaboratory-u0001 (MuPAL-u0001) in-flight simulator. The flight controller design requirements are twofold: to suppress therneffects of gusts on MuPAL-u0001 motions and to realize a wide range of maneuverability, i.e., handling characteristics,rnwithout controller redesign.Using a previously proposed two-step designmethod for two-degrees-of-freedommodel-rnmatching controllers, flight controllers were designed for the linearized longitudinal and lateral-directionalmotionsrnofMuPAL-u0001, and their performancewas examined by hardware-in-the-loop simulations and flight testswith severalrnmaneuverability models. These experiments confirmed that MuPAL-u0001 with our controllers achieves gustrnsuppression and is capable of simulating various types of handling characteristics simply by replacing themodel thatrndefines the characteristics to be examined.
机译:本文报告了多用途飞行模拟器u0001(MuPAL-u0001)飞行模拟器中飞行控制器的实验验证结果。空中控制器的设计要求是双重的:抑制阵风对MuPAL-u0001运动的影响,并实现广泛的可操纵性,即操纵特性,而无需重新设计控制器。使用先前提出的两步法两步设计方法-freedom-model-matching控制器,为线性化的纵向和横向运动设计了飞行控制器srnofMuPAL-u0001,并通过硬件在环仿真和具有多个可操纵性模型的飞行测试来检验其性能。这些实验证明,通过使用我们的控制器,MuPAL-u0001可以实现阵风抑制,并且只需替换定义了要检查的特征的模型,就可以模拟各种类型的操纵特征。

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