RU2016149727A3 - - Google Patents
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- RU2016149727A3 RU2016149727A3 RU2016149727A RU2016149727A RU2016149727A3 RU 2016149727 A3 RU2016149727 A3 RU 2016149727A3 RU 2016149727 A RU2016149727 A RU 2016149727A RU 2016149727 A RU2016149727 A RU 2016149727A RU 2016149727 A3 RU2016149727 A3 RU 2016149727A3
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Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2016149727A RU2711819C2 (en) | 2016-12-16 | 2016-12-16 | Spacecraft movement control method |
| EA201800015A EA037754B1 (en) | 2016-12-16 | 2017-12-06 | Spacecraft movement control method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2016149727A RU2711819C2 (en) | 2016-12-16 | 2016-12-16 | Spacecraft movement control method |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| RU2016149727A3 true RU2016149727A3 (en) | 2018-06-19 |
| RU2016149727A RU2016149727A (en) | 2018-06-19 |
| RU2711819C2 RU2711819C2 (en) | 2020-01-22 |
Family
ID=62619411
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2016149727A RU2711819C2 (en) | 2016-12-16 | 2016-12-16 | Spacecraft movement control method |
Country Status (2)
| Country | Link |
|---|---|
| EA (1) | EA037754B1 (en) |
| RU (1) | RU2711819C2 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109976360A (en) * | 2019-03-11 | 2019-07-05 | 北京控制工程研究所 | A kind of thruster configuration method based on configuring matrix |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5130931A (en) * | 1990-07-13 | 1992-07-14 | General Electric Company | Spacecraft attitude and velocity control system |
| RU2112713C1 (en) * | 1996-05-16 | 1998-06-10 | Ракетно-космическая корпорация "Энергия" им.С.П.Королева | Method of control of spacecraft by means of reaction actuators at maintenance of preset attitude control |
| RU2124461C1 (en) * | 1997-11-12 | 1999-01-10 | Акционерное общество открытого типа "Ракетно-космическая корпорация "Энергия" им.С.П.Королева | Method of control of space vehicle equipped with jet engines at body base line directed at angle relative to axes and thrust lines shifted relative to center of mass of vehicle; system used for realization of this method and jet engine module |
| RU2197412C2 (en) * | 2001-04-23 | 2003-01-27 | Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" им. С.П.Королева" | Method of control of spacecraft by means of powered gyroscopes and jet engines located at angle relative to axes of body base |
| RU2309876C1 (en) * | 2006-05-23 | 2007-11-10 | Федеральное государственное научное учреждение "Государственный научно-исследовательский институт прикладной механики и электродинамики" (ФГНУ "НИИ ПМЭ") | Method of control of spacecraft motion and control system for realization of this method |
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2016
- 2016-12-16 RU RU2016149727A patent/RU2711819C2/en active
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2017
- 2017-12-06 EA EA201800015A patent/EA037754B1/en unknown
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109976360A (en) * | 2019-03-11 | 2019-07-05 | 北京控制工程研究所 | A kind of thruster configuration method based on configuring matrix |
| CN109976360B (en) * | 2019-03-11 | 2021-10-01 | 北京控制工程研究所 | A thruster configuration method based on configuration matrix |
Also Published As
| Publication number | Publication date |
|---|---|
| RU2711819C2 (en) | 2020-01-22 |
| RU2016149727A (en) | 2018-06-19 |
| EA037754B1 (en) | 2021-05-18 |
| EA201800015A1 (en) | 2018-11-30 |