Patent · US Active

Method of piloting a multiple rotor rotary-wing drone to follow a curvilinear turn

US8473125B2 · kind B2 · utility

85Cited by
7References
13Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMar 1, 2012
Grant dateJun 25, 2013
Priority date
Expiry dateMar 8, 2032

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG08C2201/93
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

The respective motors of the drone (10) can be controlled to rotate at different speeds in order to pilot the drone both in attitude and speed. A remote control appliance produces a command to turn along a curvilinear path, this command comprising a left or right turning direction parameter and a parameter that defines the radius of curvature of the turn. The drone receives said command and acquires instantaneous measurements of linear velocity components, of angles of inclination, and of angular speeds of the drone. On the basis of the received command and the acquired measurements, setpoint values are generated for a control loop for controlling motors of the drone, these setpoint values controlling horizontal linear speed and inclination of the drone relative to a frame of reference associated with the ground so as to cause the drone to follow curvilinear path (C) at predetermined tangential speed (u).

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.