JP6720031B2 - 宇宙機及びその着陸方法 - Google Patents
宇宙機及びその着陸方法 Download PDFInfo
- Publication number
- JP6720031B2 JP6720031B2 JP2016175109A JP2016175109A JP6720031B2 JP 6720031 B2 JP6720031 B2 JP 6720031B2 JP 2016175109 A JP2016175109 A JP 2016175109A JP 2016175109 A JP2016175109 A JP 2016175109A JP 6720031 B2 JP6720031 B2 JP 6720031B2
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- JP
- Japan
- Prior art keywords
- spacecraft
- angle
- attitude
- aerodynamic
- attack
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Links
- 238000000034 method Methods 0.000 title claims description 31
- 230000001133 acceleration Effects 0.000 claims description 22
- 206010034719 Personality change Diseases 0.000 claims description 20
- 230000008859 change Effects 0.000 claims description 9
- 230000004044 response Effects 0.000 claims description 4
- 238000001514 detection method Methods 0.000 description 18
- 230000007246 mechanism Effects 0.000 description 15
- 238000005259 measurement Methods 0.000 description 12
- 238000010586 diagram Methods 0.000 description 5
- 238000013507 mapping Methods 0.000 description 3
- 239000003380 propellant Substances 0.000 description 2
- 241000272517 Anseriformes Species 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/244—Spacecraft control systems
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/14—Space shuttles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/244—Spacecraft control systems
- B64G1/245—Attitude control algorithms for spacecraft attitude control
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/62—Systems for re-entry into the earth's atmosphere; Retarding or landing devices
- B64G1/623—Retarding devices, e.g. retrorockets
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Radar, Positioning & Navigation (AREA)
- Automation & Control Theory (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
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 |
| US16/320,678 US20190161214A1 (en) | 2016-09-08 | 2017-08-04 | Spacecraft and landing method |
| 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 |
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 JP2018039390A5 (enExample) | 2019-09-26 |
| JP6720031B2 true JP6720031B2 (ja) | 2020-07-08 |
Family
ID=61562786
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2016175109A Active JP6720031B2 (ja) | 2016-09-08 | 2016-09-08 | 宇宙機及びその着陸方法 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US20190161214A1 (enExample) |
| EP (1) | EP3480121A4 (enExample) |
| JP (1) | JP6720031B2 (enExample) |
| WO (1) | WO2018047549A1 (enExample) |
Families Citing this family (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10800545B2 (en) * | 2015-02-23 | 2020-10-13 | Advanced Product Development, Llc | 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)
| 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. |
| CN102762456B (zh) | 2009-06-15 | 2015-11-25 | 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 |
-
2016
- 2016-09-08 JP JP2016175109A patent/JP6720031B2/ja active Active
-
2017
- 2017-08-04 US US16/320,678 patent/US20190161214A1/en not_active Abandoned
- 2017-08-04 EP EP17848493.7A patent/EP3480121A4/en not_active Withdrawn
- 2017-08-04 WO PCT/JP2017/028439 patent/WO2018047549A1/ja not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| WO2018047549A1 (ja) | 2018-03-15 |
| EP3480121A1 (en) | 2019-05-08 |
| EP3480121A4 (en) | 2020-02-19 |
| US20190161214A1 (en) | 2019-05-30 |
| JP2018039390A (ja) | 2018-03-15 |
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