Rotorcraft control system, associated rotorcraft, and corresponding control method
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United States of America Patent
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Mar 13, 2018
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N/A
app pub date -
May 4, 2016
filing date -
May 4, 2015
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Abstract
A control system for a rotorcraft, which system includes at least one control unit allowing a rotor of a rotorcraft to be driven, with the rotorcraft including at least three independent landing-gear units, with each landing-gear unit including means for detecting a ground reaction force F1, F2, F3 exerted on the landing-gear unit when the rotorcraft is in contact with the ground, and with the control system being suitable for receiving information from the detection means. The invention also relates to the rotorcraft and to a control method corresponding to the control system.
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