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1. (WO2017013842) UNMANNED FLIGHT VEHICLE, FLIGHT CONTROL METHOD, AND FLIGHT CONTROL PROGRAM
Latest bibliographic data on file with the International Bureau   

Pub. No.: WO/2017/013842 International Application No.: PCT/JP2016/003144
Publication Date: 26.01.2017 International Filing Date: 30.06.2016
IPC:
G05D 1/10 (2006.01) ,B64C 13/18 (2006.01) ,B64C 39/02 (2006.01) ,B64D 27/24 (2006.01) ,G01C 21/26 (2006.01) ,G08G 5/00 (2006.01)
G PHYSICS
05
CONTROLLING; REGULATING
D
SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
1
Control of position, course, altitude, or attitude of land, water, air, or space vehicles, e.g. automatic pilot
10
Simultaneous control of position or course in three dimensions
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
13
Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
02
Initiating means
16
actuated automatically, e.g. responsive to gust detectors
18
using automatic pilot
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
39
Aircraft not otherwise provided for
02
characterised by special use
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
D
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS
27
Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
02
Aircraft characterised by the type or position of power plant
24
using steam, electricity, or spring force
G PHYSICS
01
MEASURING; TESTING
C
MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
21
Navigation; Navigational instruments not provided for in groups G01C1/-G01C19/104
26
specially adapted for navigation in a road network
G PHYSICS
08
SIGNALLING
G
TRAFFIC CONTROL SYSTEMS
5
Traffic control systems for aircraft
Applicants:
パナソニック インテレクチュアル プロパティ コーポレーション オブ アメリカ PANASONIC INTELLECTUAL PROPERTY CORPORATION OF AMERICA [US/US]; カリフォルニア州トーランス,スイート 200,マリナー アベニュー 20000 20000 Mariner Avenue, Suite 200, Torrance, California 90503, US
Inventors:
久原 俊介 KUHARA, Shunsuke; JP
Agent:
徳田 佳昭 TOKUDA, Yoshiaki; JP
Priority Data:
2015-21033227.10.2015JP
2016-12324422.06.2016JP
62/193,67017.07.2015US
Title (EN) UNMANNED FLIGHT VEHICLE, FLIGHT CONTROL METHOD, AND FLIGHT CONTROL PROGRAM
(FR) VÉHICULE AÉRIEN SANS PILOTE, PROCÉDÉ DE COMMANDE DE VOL ET PROGRAMME DE COMMANDE DE VOL
(JA) 無人飛行体、飛行制御方法及び飛行制御プログラム
Abstract:
(EN) This unmanned flight vehicle (10) comprises: a remaining battery capacity acquisition unit (112) that acquires the remaining capacity of a battery (106); an arrival determination unit (114) that determines, when the unmanned flight vehicle (10) starts to move from a first point where the vehicle is currently located to a second point where the unmanned flight vehicle (10) passes subsequent to the first point, whether or not the unmanned flight vehicle (10) is capable of arriving at the second point on the basis of the remaining capacity of the battery (106) and the end time of a time period during which the unmanned flight vehicle (10) is permitted to fly; and a flight control unit (111) that causes the unmanned flight vehicle (10) to depart toward the second point in cases where it is determined that the unmanned flight vehicle (10) is capable of arriving at the second point.
(FR) La présente invention concerne un véhicule aérien sans pilote (10) qui comprend : une unité d'acquisition de capacité restante de batterie (112) qui acquiert la capacité restante d'une batterie (106) ; une unité de détermination d'arrivée (114) qui détermine, lorsque le véhicule aérien sans pilote (10) commence à se déplacer d'un premier point où le véhicule est actuellement situé, jusqu'à un second point où le véhicule aérien sans pilote (10) passe après le premier point, si le véhicule aérien sans pilote (10) peut, ou non, arriver au second point sur la base de la capacité restante de la batterie (106) ainsi que l'heure de fin d'une période de temps pendant laquelle le véhicule aérien sans pilote (10) est autorisé à voler ; et une unité de commande de vol (111) qui provoque le départ du véhicule aérien sans pilote (10) vers le second point dans les cas où il est déterminé que le véhicule aérien sans pilote (10) peut arriver au second point.
(JA) 無人飛行体(10)は、バッテリ(106)の残容量を取得するバッテリ残容量取得部(112)と、無人飛行体(10)が現在位置する第1の地点から、第1の地点の次に無人飛行体(10)が経由する第2の地点に移動を開始する際、無人飛行体(10)の飛行が許可されている時間帯の終了時刻と、バッテリ(106)の残容量とに基づいて、無人飛行体(10)が第2の地点に到着可能であるか否かを判断する到着判断部(114)と、無人飛行体(10)が第2の地点に到着可能であると判断された場合、無人飛行体(10)を第2の地点へ向けて出発させる飛行制御部(111)とを備える。
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Designated States: AE, AG, AL, AM, AO, AT, AU, AZ, BA, BB, BG, BH, BN, BR, BW, BY, BZ, CA, CH, CL, CN, CO, CR, CU, CZ, DE, DK, DM, DO, DZ, EC, EE, EG, ES, FI, GB, GD, GE, GH, GM, GT, HN, HR, HU, ID, IL, IN, IR, IS, KE, KG, KN, KP, KR, KZ, LA, LC, LK, LR, LS, LU, LY, MA, MD, ME, MG, MK, MN, MW, MX, MY, MZ, NA, NG, NI, NO, NZ, OM, PA, PE, PG, PH, PL, PT, QA, RO, RS, RU, RW, SA, SC, SD, SE, SG, SK, SL, SM, ST, SV, SY, TH, TJ, TM, TN, TR, TT, TZ, UA, UG, US, UZ, VC, VN, ZA, ZM, ZW
African Regional Intellectual Property Organization (ARIPO) (BW, GH, GM, KE, LR, LS, MW, MZ, NA, RW, SD, SL, ST, SZ, TZ, UG, ZM, ZW)
Eurasian Patent Office (AM, AZ, BY, KG, KZ, RU, TJ, TM)
European Patent Office (EPO) (AL, AT, BE, BG, CH, CY, CZ, DE, DK, EE, ES, FI, FR, GB, GR, HR, HU, IE, IS, IT, LT, LU, LV, MC, MK, MT, NL, NO, PL, PT, RO, RS, SE, SI, SK, SM, TR)
African Intellectual Property Organization (BF, BJ, CF, CG, CI, CM, GA, GN, GQ, GW, KM, ML, MR, NE, SN, TD, TG)
Publication Language: Japanese (JA)
Filing Language: Japanese (JA)