Investigation of a robust tendon-sheath mechanism for flexible membrane wing application in mini-UAV
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文摘
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A flexible wing morphing to cater for gusty-proof mini-UAVs is developed.

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Tendon-sheath mechanism is utilized for the actuation.

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The dynamics of the tendon-sheath mechanism is characterized and modeled.

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A model based control strategy to regulate the wing actuation is implemented.

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The system is validated satisfactorily on a wind tunnel with gusty scenario.

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