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1. WO2020066549 - CONTROL DEVICE, CONTROL METHOD, AND PROGRAM

Publication Number WO/2020/066549
Publication Date 02.04.2020
International Application No. PCT/JP2019/035144
International Filing Date 06.09.2019
IPC
G05D 1/10 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
10Simultaneous control of position or course in three dimensions
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
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
G05D 1/10
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
10Simultaneous control of position or course in three dimensions
Applicants
  • 日本電気株式会社 NEC CORPORATION [JP]/[JP]
Inventors
  • オウ シンイ WANG Zhenwei
Agents
  • 速水 進治 HAYAMI Shinji
Priority Data
2018-18055226.09.2018JP
Publication Language Japanese (JA)
Filing Language Japanese (JA)
Designated States
Title
(EN) CONTROL DEVICE, CONTROL METHOD, AND PROGRAM
(FR) DISPOSITIF DE COMMANDE, PROCÉDÉ DE COMMANDE ET PROGRAMME
(JA) 制御装置、制御方法、及びプログラム
Abstract
(EN)
Provided is a control device (2000) including a first mode and a second mode as control modes related to control of a flying body. The first mode is a control mode for accurately controlling the position of an arm (20). Thus, when the control mode of the flying body (10) is the first mode, the control device (2000) performs flying control on the flying body (10) by giving priority to a first position (30) that is a position on the arm (20). On the other hand, the second mode is a mode different from the first mode. When the control mode of the flying body (10) is the second mode, the control device (2000) performs flying control on the flying body (10) by giving priority to a second position (40) that is a reference position other than the positions on the arm (20). For example, the second position is the center of a fuselage.
(FR)
La présente invention concerne un dispositif de commande (2000) comprenant un premier mode et un second mode en tant que modes de commande associés à la commande d'un corps volant. Le premier mode est un mode de commande permettant de commander avec précision la position d'un bras (20). Ainsi, lorsque le mode de commande du corps volant (10) est le premier mode, le dispositif de commande (2000) réalise une commande de vol sur le corps volant (10) en donnant priorité à une première position (30) qui est une position sur le bras (20). D'autre part, le second mode est un mode différent du premier mode. Lorsque le mode de commande du corps volant (10) est le second mode, le dispositif de commande (2000) réalise une commande de vol sur le corps volant (10) en donnant priorité à une seconde position (40) qui est une position de référence différente des positions sur le bras (20). Par exemple, la seconde position est le centre d'un fuselage.
(JA)
制御装置(2000)では、飛翔体の制御に関する制御モードとして、第1モードと第2モードが存在する。第1モードは、アーム(20)の位置を正確に制御するための制御モードである。そのため、制御装置(2000)は、飛翔体(10)の制御モードが第1モードである場合、アーム(20)上の位置である第1位置(30)を優先して、飛翔(10)の飛行制御を行う。一方、第2モードは、第1モードとは異なるモードである。制御装置(2000)は、飛翔体(10)の制御モードが第2モードである場合、アーム(20)上の位置以外の基準位置である第2位置(40)を優先して、飛翔体(10)の飛行制御を行う。例えば第2位置は機体中心である。
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