JP2018039390A5 - - Google Patents

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Publication number
JP2018039390A5
JP2018039390A5 JP2016175109A JP2016175109A JP2018039390A5 JP 2018039390 A5 JP2018039390 A5 JP 2018039390A5 JP 2016175109 A JP2016175109 A JP 2016175109A JP 2016175109 A JP2016175109 A JP 2016175109A JP 2018039390 A5 JP2018039390 A5 JP 2018039390A5
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JP
Japan
Prior art keywords
spacecraft
angle
attitude
aerodynamic
control device
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JP2016175109A
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English (en)
Japanese (ja)
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JP2018039390A (ja
JP6720031B2 (ja
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Priority to JP2016175109A priority Critical patent/JP6720031B2/ja
Priority claimed from JP2016175109A external-priority patent/JP6720031B2/ja
Priority to EP17848493.7A priority patent/EP3480121A4/en
Priority to PCT/JP2017/028439 priority patent/WO2018047549A1/ja
Priority to US16/320,678 priority patent/US20190161214A1/en
Publication of JP2018039390A publication Critical patent/JP2018039390A/ja
Publication of JP2018039390A5 publication Critical patent/JP2018039390A5/ja
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Publication of JP6720031B2 publication Critical patent/JP6720031B2/ja
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JP2016175109A 2016-09-08 2016-09-08 宇宙機及びその着陸方法 Active JP6720031B2 (ja)

Priority Applications (4)

Application Number Priority Date Filing Date Title
JP2016175109A JP6720031B2 (ja) 2016-09-08 2016-09-08 宇宙機及びその着陸方法
EP17848493.7A EP3480121A4 (en) 2016-09-08 2017-08-04 SPACING MACHINE AND LANDING METHOD THEREOF
PCT/JP2017/028439 WO2018047549A1 (ja) 2016-09-08 2017-08-04 宇宙機及びその着陸方法
US16/320,678 US20190161214A1 (en) 2016-09-08 2017-08-04 Spacecraft and landing method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2016175109A JP6720031B2 (ja) 2016-09-08 2016-09-08 宇宙機及びその着陸方法

Publications (3)

Publication Number Publication Date
JP2018039390A JP2018039390A (ja) 2018-03-15
JP2018039390A5 true JP2018039390A5 (enExample) 2019-09-26
JP6720031B2 JP6720031B2 (ja) 2020-07-08

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JP2016175109A Active JP6720031B2 (ja) 2016-09-08 2016-09-08 宇宙機及びその着陸方法

Country Status (4)

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US (1) US20190161214A1 (enExample)
EP (1) EP3480121A4 (enExample)
JP (1) JP6720031B2 (enExample)
WO (1) WO2018047549A1 (enExample)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016137877A1 (en) * 2015-02-23 2016-09-01 Advanced Aerospace Technologies, Inc. Rocket landing system
CN109579833B (zh) * 2018-12-04 2020-07-17 上海航天控制技术研究所 一种对返回式运载火箭的垂直着陆阶段的组合导航方法
CN110667890B (zh) * 2019-09-10 2022-06-28 北方信息控制研究院集团有限公司 一种空间飞行器非线性姿态稳定方法
WO2021242474A2 (en) * 2020-05-03 2021-12-02 Advanced Product Development, Llc Rocket launching and landing system
JP7465531B2 (ja) * 2020-07-17 2024-04-11 国立研究開発法人宇宙航空研究開発機構 ロケット制御システム、及びロケットの着陸動作の制御方法
CN112249369B (zh) * 2020-09-28 2022-01-04 上海航天控制技术研究所 一种火箭动力定点着陆制导方法
FR3116512B1 (fr) * 2020-11-25 2024-09-20 Arianegroup Sas Système de transport spatial réutilisable
CN112525004B (zh) * 2020-11-27 2022-10-18 中国人民解放军国防科技大学 火箭定点软着陆的开机点在线确定方法及系统
FR3121125B1 (fr) * 2021-03-23 2024-05-03 Arianegroup Sas Système de transport hypersonique
CN114690793B (zh) * 2022-03-28 2023-01-06 北京理工大学 基于滑模控制的可重复使用运载火箭垂直软着陆制导方法

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070012820A1 (en) * 2004-08-11 2007-01-18 David Buehler Reusable upper stage
FR2907422B1 (fr) 2006-10-20 2009-12-18 Astrium Sas Aeronef a vol mixte aerodynamique et spatial, et procede de pilotage associe.
CN105398583B (zh) 2009-06-15 2017-11-14 蓝源有限责任公司 太空运载火箭海上着陆及相关的系统和方法
US8571727B1 (en) * 2013-02-06 2013-10-29 The Aerospace Corporation Energy-angular momentum closed-loop guidance for launch vehicles
JP6432903B2 (ja) * 2014-09-26 2018-12-05 三菱重工業株式会社 垂直離着陸機、及び垂直離着陸機の制御方法
JP6452513B2 (ja) 2015-03-20 2019-01-16 株式会社キーエンス レーザマーキング装置、該レーザマーキング装置を用いた印字方法及びコンピュータプログラム

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