JP6517104B2 - 航空機管理装置、航空機、及び航空機の軌道算出方法 - Google Patents

航空機管理装置、航空機、及び航空機の軌道算出方法 Download PDF

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Publication number
JP6517104B2
JP6517104B2 JP2015143183A JP2015143183A JP6517104B2 JP 6517104 B2 JP6517104 B2 JP 6517104B2 JP 2015143183 A JP2015143183 A JP 2015143183A JP 2015143183 A JP2015143183 A JP 2015143183A JP 6517104 B2 JP6517104 B2 JP 6517104B2
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Prior art keywords
aircraft
role
constraint
objective function
trajectory
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Japanese (ja)
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JP2017026190A (ja
JP2017026190A5 (https=
Inventor
光一 山崎
光一 山崎
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Mitsubishi Heavy Industries Ltd
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Mitsubishi Heavy Industries Ltd
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Priority to JP2015143183A priority Critical patent/JP6517104B2/ja
Priority to PCT/JP2016/070413 priority patent/WO2017014085A1/ja
Priority to EP16827646.7A priority patent/EP3255371B1/en
Priority to US15/561,645 priority patent/US10627834B2/en
Publication of JP2017026190A publication Critical patent/JP2017026190A/ja
Publication of JP2017026190A5 publication Critical patent/JP2017026190A5/ja
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C19/00—Aircraft control not otherwise provided for
    • B64C19/02—Conjoint controls
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/12—Target-seeking control
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G9/00—Systems for controlling missiles or projectiles, not provided for elsewhere
    • F41G9/002—Systems for controlling missiles or projectiles, not provided for elsewhere for guiding a craft to a correct firing position
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H13/00—Means of attack or defence not otherwise provided for
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0005—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with arrangements to save energy
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0094—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots involving pointing a payload, e.g. camera, weapon, sensor, towards a fixed or moving target
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/10—Simultaneous control of position or course in three dimensions
    • G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
    • G05D1/104—Simultaneous control of position or course in three dimensions specially adapted for aircraft involving a plurality of aircrafts, e.g. formation flying
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/10—Simultaneous control of position or course in three dimensions
    • G05D1/107—Simultaneous control of position or course in three dimensions specially adapted for missiles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/24—Beam riding guidance systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/30—Command link guidance systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • General Engineering & Computer Science (AREA)
  • Traffic Control Systems (AREA)
JP2015143183A 2015-07-17 2015-07-17 航空機管理装置、航空機、及び航空機の軌道算出方法 Active JP6517104B2 (ja)

Priority Applications (4)

Application Number Priority Date Filing Date Title
JP2015143183A JP6517104B2 (ja) 2015-07-17 2015-07-17 航空機管理装置、航空機、及び航空機の軌道算出方法
PCT/JP2016/070413 WO2017014085A1 (ja) 2015-07-17 2016-07-11 航空機管理装置、航空機、及び航空機の軌道算出方法
EP16827646.7A EP3255371B1 (en) 2015-07-17 2016-07-11 Aircraft control device, aircraft, and method for computing aircraft trajectory
US15/561,645 US10627834B2 (en) 2015-07-17 2016-07-11 Aircraft control device, aircraft, and method for computing aircraft trajectory

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2015143183A JP6517104B2 (ja) 2015-07-17 2015-07-17 航空機管理装置、航空機、及び航空機の軌道算出方法

Publications (3)

Publication Number Publication Date
JP2017026190A JP2017026190A (ja) 2017-02-02
JP2017026190A5 JP2017026190A5 (https=) 2018-06-14
JP6517104B2 true JP6517104B2 (ja) 2019-05-22

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JP2015143183A Active JP6517104B2 (ja) 2015-07-17 2015-07-17 航空機管理装置、航空機、及び航空機の軌道算出方法

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Country Link
US (1) US10627834B2 (https=)
EP (1) EP3255371B1 (https=)
JP (1) JP6517104B2 (https=)
WO (1) WO2017014085A1 (https=)

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US9678506B2 (en) 2014-06-19 2017-06-13 Skydio, Inc. Magic wand interface and other user interaction paradigms for a flying digital assistant
US9798322B2 (en) 2014-06-19 2017-10-24 Skydio, Inc. Virtual camera interface and other user interaction paradigms for a flying digital assistant
US12007763B2 (en) 2014-06-19 2024-06-11 Skydio, Inc. Magic wand interface and other user interaction paradigms for a flying digital assistant
US9564056B1 (en) * 2015-09-03 2017-02-07 General Electric Company Flight path optimization using nonlinear programming
US10435176B2 (en) 2016-05-25 2019-10-08 Skydio, Inc. Perimeter structure for unmanned aerial vehicle
US10520943B2 (en) 2016-08-12 2019-12-31 Skydio, Inc. Unmanned aerial image capture platform
US11295458B2 (en) 2016-12-01 2022-04-05 Skydio, Inc. Object tracking by an unmanned aerial vehicle using visual sensors
CN107121015B (zh) * 2017-06-16 2018-10-16 湖北航天技术研究院总体设计所 一种快速弹上弹道在线规划方法
CN109186611B (zh) * 2018-10-31 2020-09-15 南京航空航天大学 无人机飞行路径分配方法及装置
CN109840916B (zh) * 2019-01-22 2019-12-13 中国海洋大学 高频地波雷达舰船目标跟踪算法的测评方法
US11573577B2 (en) * 2019-01-30 2023-02-07 The Government Of The United States Of America, As Represented By The Secretary Of The Navy Method and system for optimal trajectory path tasking for an unmanned aerial vehicle (UAV)
CN110470306B (zh) * 2019-08-27 2023-03-10 中山大学 一种可保证连通性约束的基于深度强化学习的多机器人编队导航方法
CN111045447B (zh) * 2019-11-21 2023-08-29 浙江大学 高精度的高超声速飞行器轨迹优化多尺度最优控制系统
CN113093716B (zh) * 2019-12-19 2024-04-30 广州极飞科技股份有限公司 一种运动轨迹规划方法、装置、设备及存储介质
CN113221389B (zh) * 2021-06-17 2023-08-08 中国人民解放军火箭军工程大学 一种飞行器发射时间筹划方法及系统
CN114510067B (zh) * 2022-01-28 2024-07-19 北京航空航天大学 一种可重复使用飞行器近似最优制导方法
CN115145295B (zh) * 2022-07-13 2024-10-29 西北工业大学 一种动态环境下无人机在线自主航迹优化控制方法
CN115469676B (zh) * 2022-07-26 2025-02-07 西南科技大学 结合伯克霍夫插值和lgl伪谱法的飞行器轨迹优化方法
CN115327499B (zh) * 2022-08-16 2023-09-22 扬州宇安电子科技有限公司 一种基于载荷无人机的雷达目标航迹模拟方法
CN116513467B (zh) * 2023-04-27 2023-12-26 华中科技大学 一种考虑进气安全的高速飞行器优化控制方法
CN118609725B (zh) * 2024-05-31 2025-02-11 西南石油大学 一种超深裂缝性储层承压堵漏体系智能设计方法

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US20040068351A1 (en) * 2002-04-22 2004-04-08 Neal Solomon System, methods and apparatus for integrating behavior-based approach into hybrid control model for use with mobile robotic vehicles
JP2004025966A (ja) * 2002-06-24 2004-01-29 Mitsubishi Heavy Ind Ltd 航空機の機動選択システム
FR2897959B1 (fr) * 2006-02-28 2008-04-04 Airbus France Sas Dispositif d'aide au guidage d'un aeronef suiveur faisant partie d'une patrouille, ainsi qu'un systeme d'aide a un vol en patrouille comportant un tel dispositif.
ATE514986T1 (de) * 2007-10-15 2011-07-15 Saab Ab Verfahren und vorrichtung zur erzeugung mindestens einer gewählten flugbahn eines fahrzeugs
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JP5748506B2 (ja) * 2011-02-28 2015-07-15 三菱重工業株式会社 管制装置、航空機、及び管制方法
JP6207908B2 (ja) 2012-11-29 2017-10-04 三菱重工業株式会社 航空機管理装置、航空機、及び航空機管理方法
FR3021107B1 (fr) * 2014-05-16 2018-01-26 Thales Procede d'aide a la navigation d'un aeronef avec correlation d'informations dynamiques avec une trajectoire de vol 4d

Also Published As

Publication number Publication date
EP3255371B1 (en) 2020-01-29
JP2017026190A (ja) 2017-02-02
US20180074524A1 (en) 2018-03-15
EP3255371A4 (en) 2018-01-17
EP3255371A1 (en) 2017-12-13
US10627834B2 (en) 2020-04-21
WO2017014085A1 (ja) 2017-01-26

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