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公开(公告)号:US20170361927A1
公开(公告)日:2017-12-21
申请号:US15628402
申请日:2017-06-20
Applicant: PARROT DRONES
Inventor: Gauthier Lavagen , Marc MARI MARI , Yoni BENATAR , Thomas BARSE
CPC classification number: B64C27/26 , A63H27/12 , B64C3/32 , B64C11/46 , B64C29/0025 , B64C29/02 , B64C39/024 , B64C39/08 , B64C2201/02 , B64C2201/042 , B64C2201/088 , B64C2201/104 , B64C2201/108 , B64C2201/146 , B64C2201/165 , B64C2201/187
Abstract: A rotary-wing drone includes a drone body that includes an electronic board controlling the piloting of the drone, and four link arms that include a rigidly connected propulsion unit. The link arms form lift-producing wings.
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公开(公告)号:US20170364093A1
公开(公告)日:2017-12-21
申请号:US15628541
申请日:2017-06-20
Applicant: PARROT DRONES
Inventor: Marc Mari Mari , Gauthier Lavagen , Yoni Benatar
CPC classification number: G05D1/0825 , B64C13/16 , B64C27/26 , B64C39/024 , B64C2201/088 , B64C2201/104 , B64C2201/108 , B64C2201/14 , B64C2201/165 , G05D1/0202 , G05D1/0808 , G05D1/085 , G05D1/0858
Abstract: A method for dynamically controlling the attitude of a rotary-wing drone. The method includes dynamically controlling the attitude of the drone when the drone is flying using lift of each of four wings of the drone, by controlling the attitude of the drone by sending differentiated commands to one or more propulsion units of the drone so as to rotate the drone about a roll axis and/or pitch axis and/or heading axis of the drone from a current angular position to a final angular position, the axes being defined in the reference point of the drone.
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