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1. WO2020110293 - DISPLAY CONTROL SYSTEM, DISPLAY CONTROL DEVICE, AND DISPLAY CONTROL METHOD

Publication Number WO/2020/110293
Publication Date 04.06.2020
International Application No. PCT/JP2018/044182
International Filing Date 30.11.2018
IPC
B64D 45/00 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
45Aircraft indicators or protectors not otherwise provided for
B64C 13/20 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
13Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
02Initiating means
16actuated automatically, e.g. responsive to gust detectors
20using radiated signals
B64C 39/02 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
39Aircraft not otherwise provided for
02characterised by special use
B64D 47/08 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
47Equipment not otherwise provided for
08Arrangements of cameras
G05D 1/00 2006.01
GPHYSICS
05CONTROLLING; REGULATING
DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
1Control of position, course, altitude, or attitude of land, water, air, or space vehicles, e.g. automatic pilot
CPC
B64C 13/20
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
13Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
02Initiating means
16actuated automatically, e.g. responsive to gust detectors
20using radiated signals
B64C 39/02
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
39Aircraft not otherwise provided for
02characterised by special use
B64D 45/00
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
45Aircraft indicators or protectors not otherwise provided for
B64D 47/08
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
47Equipment not otherwise provided for
08Arrangements of cameras
G05D 1/00
GPHYSICS
05CONTROLLING; REGULATING
DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
1Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
Applicants
  • 楽天株式会社 RAKUTEN, INC. [JP]/[JP]
Inventors
  • 中澤 満 NAKAZAWA, Mitsuru
  • 岩瀬 裕章 IWASE, Hiroaki
Agents
  • 特許業務法人はるか国際特許事務所 HARUKA PATENT & TRADEMARK ATTORNEYS
Priority Data
Publication Language Japanese (JA)
Filing Language Japanese (JA)
Designated States
Title
(EN) DISPLAY CONTROL SYSTEM, DISPLAY CONTROL DEVICE, AND DISPLAY CONTROL METHOD
(FR) SYSTÈME DE COMMANDE D'AFFICHAGE, DISPOSITIF DE COMMANDE D'AFFICHAGE ET PROCÉDÉ DE COMMANDE D'AFFICHAGE
(JA) 表示制御システム、表示制御装置及び表示制御方法
Abstract
(EN)
Provided are a display control system, a display control device, and a display control method that enable the display state of images captured by a camera of an unmanned aerial vehicle to be suitably controlled. A sensing data acquiring unit (60) acquires the aerial-vehicle-captured images captured by the camera of the unmanned aerial vehicle when in flight. A determination unit (62) determines whether an operator of the unmanned aerial vehicle is viewing the unmanned aerial vehicle on the basis of sensing data relating to the unmanned aerial vehicle and/or relating the operator. A display control unit (64) controls the display state of the aerial-vehicle-captured images on a display unit, according to whether a determination that the operator is not viewing the unmanned aerial vehicle continues.
(FR)
L'invention concerne un système de commande d'affichage, un dispositif de commande d'affichage et un procédé de commande d'affichage qui permettent de commander de manière appropriée l'état d'affichage d'images capturées par une caméra d'un aéronef sans pilote. Une unité d'acquisition de données de détection (60) acquiert les images capturées par un aéronef capturées par la caméra de l'aéronef sans pilote lorsqu'il est en vol. Une unité de détermination (62) détermine si un opérateur de l'aéronef sans pilote voit l'aéronef sans pilote sur la base de données de détection relatives à l'aéronef sans pilote et/ou concernant l'opérateur. Une unité de commande d'affichage (64) commande l'état d'affichage des images capturées par l'aéronef sur une unité d'affichage, selon qu'une détermination selon laquelle l'opérateur ne voit pas l'aéronef sans pilote se poursuit.
(JA)
無人航空機が備えたカメラが撮影する画像の表示状態を適切に制御できる表示制御システム、表示制御装置及び表示制御方法を提供する。センシングデータ取得部(60)は、飛行中の無人航空機が備えるカメラにより撮影される航空機撮影画像を取得する。判定部(62)は、無人航空機及び当該無人航空機の操縦者のうちの少なくとも一方に関するセンシングデータに基づいて、当該無人航空機を当該操縦者が目視しているか否かを判定する。表示制御部(64)は、無人航空機を操縦者が目視していないとの判定が継続しているか否かに応じて、表示部における前記航空機撮影画像の表示状態を制御する。
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