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- W2088305932 abstract "This paper investigates the capabilities of the SimMechanics Simulink multibody modelling tool in analysing the dynamic and shape changing response of morphing aircraft. The research is focused on morphing aircraft that undergo large discrete shape variation in which the “morphing” is due to a set of rigid bodies moving relative to each other. The aerodynamic loads contribution is calculated via a quasi-steady linear vortex-lattice code that has been implemented within the Matlab-Simulink environment in order to be directly linked to the SimMechanics block. The methodology is applied to an actual morphing aircraft demonstrator that is a flying wing based on an “active winglets” concept which means that manoeuvres are controlled by a two degrees of freedom tilting-wing-tip system. Particular attention is given to the effects of the variation in the shape on the inertia properites, the centre of gravity location and modal parameters. Finally a response simulation with respect to a time change in shape input is discussed." @default.
- W2088305932 created "2016-06-24" @default.
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- W2088305932 date "2007-06-15" @default.
- W2088305932 modified "2023-09-28" @default.
- W2088305932 title "Modelling the Dynamic Response of a Morphing Wing with Active Winglets" @default.
- W2088305932 cites W2085265384 @default.
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- W2088305932 doi "https://doi.org/10.2514/6.2007-6500" @default.
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