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Title:
METHOD OF PILOTING MULTIPLE ROTOR ROTARY-WING DRONE TO FOLLOW CURVILINEAR TURN
Document Type and Number:
Japanese Patent JP2012198883
Kind Code:
A
Abstract:

To provide a mode of controlling a drone that enables it to fly over typical turning paths.

Respective motors of a 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 (16) produces a command to turn along a curvilinear path, and the command comprises a left or right turning direction parameter and a parameter that defines the radius of curvature of the turn. The drone receives the 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, set-point values are generated for a control loop for controlling motors of the drone, and the set-point values control 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 the curvilinear path at a predetermined tangential speed (u).


Inventors:
FREDERIC D'HAEYER
MICHAEL RISCHMULLER
Application Number:
JP2012051103A
Publication Date:
October 18, 2012
Filing Date:
March 08, 2012
Export Citation:
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Assignee:
PARROT
International Classes:
G05D1/08; B64C27/08; B64C29/00; G05D1/00
Domestic Patent References:
JP2009515771A2009-04-16
JP2008092818A2008-04-24
JPH09145367A1997-06-06
JP2005329255A2005-12-02
JP2001142862A2001-05-25
JP2004256022A2004-09-16
JP2002211494A2002-07-31
JP2006312344A2006-11-16
Foreign References:
WO2010061099A22010-06-03
US20020104921A12002-08-08
US20110049290A12011-03-03
US20020060267A12002-05-23
Attorney, Agent or Firm:
内田 浩輔
岡部 讓
松井 孝夫
越智 隆夫
高橋 誠一郎