Variable damping of haptic feedback for kinematic linkage to change the flight attitude of an aircraft
作者： Julien Pruss , Bernard Gemmati , Romuald Biest
DOI:
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摘要: The method involves damping operations of a manual flight control device by haptic feedback defined according to predetermined force relationship (A). is as function an instantaneous load factor hybrid helicopter (1) so that maintained between its minimum and maximum limit values in proportion position thrust unit (20) (22) (23). An independent claim also included for including damper implementing the providing feedback.
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