ES2044189T3 - Procedimiento de determinacion y de control de la posicion de un satelite por autorrotacion eliptica de transferencia. - Google Patents
Procedimiento de determinacion y de control de la posicion de un satelite por autorrotacion eliptica de transferencia.Info
- Publication number
- ES2044189T3 ES2044189T3 ES89403387T ES89403387T ES2044189T3 ES 2044189 T3 ES2044189 T3 ES 2044189T3 ES 89403387 T ES89403387 T ES 89403387T ES 89403387 T ES89403387 T ES 89403387T ES 2044189 T3 ES2044189 T3 ES 2044189T3
- Authority
- ES
- Spain
- Prior art keywords
- satellite
- behavior
- control
- apogeo
- maneuver
- 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.)
- Expired - Lifetime
Links
- 238000005259 measurement Methods 0.000 abstract 1
Classifications
-
- 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
- B64G1/281—Spin-stabilised spacecraft
-
- 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
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
-
- 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
- B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
- B64G1/363—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using sun sensors
-
- 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
- B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
- B64G1/365—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using horizon or Earth sensors
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Radar, Positioning & Navigation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Navigation (AREA)
- Management, Administration, Business Operations System, And Electronic Commerce (AREA)
Abstract
PARA CONTROLAR EL COMPORTAMIENTO DE UN SATELITE (1) ESTABILIZADO POR AUTORROTACION EN UNA ORBITA ELECTRICA DE TRANSFERENCIA (7) PARA QUE PASE POR UNA ORBITA ESTACIONARIA, TRAS INYECTAR EL SATELITE EN LA ORBITA DE TRANSFERENCIA EN EL PERIFEO DE LA MISMA, CON UN COMPORTAMIENTO INICIAL PROXIMO AL COMPORTAMIENTO FINAL PREDETERMINADO PARA LA MANIOBRA DE APOGEO: - SE MODIFICA (C) LA ASCENSION RECTA (BETA) DEL SATELITE DE FORMA QUE SE LE CONFIERA UN COMPORTAMIENTO INTERMEDIO, COMO QUE EL CAMPO DE VISION DE LOS DETECTORES TERRESTRES (5) INTERCEPTE A LA TIERRA PARA UNA POSICION DEL SATELITE EN LA ORBITA DE TRANSFERENCIA DESFASADA EN AL MENOS 10 GRADOS EN RELACION AL APOGEO; - SE MIDE LA DECLINACION (ALFA) DEL EJE DE ROTACION DEL SATELITE, DESPUES SE AJUSTA (C'') AL VALOR DESEADO PARA LA MANIOBRA DE APOGEO; - MANTENIENDO ESTA DECLINACION CONSTANTE, SE AJUSTA (D) LA ASCENSION RECTA A PARTIR DE LAS MEDICIONES DE LOS DETECTORES SOLARES DE FORMA QUE SE LLEVE AL SATELITE A SU COMPORTAMIENTO FINAL; Y - SECONTROLA MANIOBRA DE APOGEO.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8817120A FR2640933B1 (es) | 1988-12-23 | 1988-12-23 |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2044189T3 true ES2044189T3 (es) | 1994-01-01 |
Family
ID=9373377
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES89403387T Expired - Lifetime ES2044189T3 (es) | 1988-12-23 | 1989-12-06 | Procedimiento de determinacion y de control de la posicion de un satelite por autorrotacion eliptica de transferencia. |
Country Status (7)
Country | Link |
---|---|
US (1) | US5064152A (es) |
EP (1) | EP0375496B1 (es) |
JP (1) | JPH02237897A (es) |
CA (1) | CA2005025A1 (es) |
DE (1) | DE68909389T2 (es) |
ES (1) | ES2044189T3 (es) |
FR (1) | FR2640933B1 (es) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112537461A (zh) * | 2020-12-03 | 2021-03-23 | 北京航空航天大学 | 一种基于星载关联性健康基线卫星在轨实时监测方法 |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5251855A (en) * | 1990-05-09 | 1993-10-12 | Agence Spatiale Europeenne | Spacecraft propulsion system thruster firing system |
AU6649798A (en) | 1997-02-04 | 1998-08-25 | Edward A. Belbruno | New procedure for generating operational ballistic capture transfer using a computer implemented process |
US6097997A (en) * | 1997-03-25 | 2000-08-01 | Galaxy Development, Llc | Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same |
AU7357198A (en) | 1997-03-25 | 1998-10-20 | Edward A. Belbruno | Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same |
WO1998047765A1 (en) | 1997-04-24 | 1998-10-29 | Galaxy Development, Llc. | Satellite inclination changes using weak stability boundaries |
US6385512B1 (en) | 1999-04-16 | 2002-05-07 | Galaxy Development Llc | System and method of a ballistic capture transfer to L4, L5 |
US7090171B2 (en) | 2003-01-14 | 2006-08-15 | Honeywell International, Inc. | Momentum stabilized launch vehicle upper stage |
KR20070073273A (ko) * | 2006-01-04 | 2007-07-10 | 삼성전자주식회사 | 휴대용 단말기에서 폴더의 회전 상태를 감지하는 장치 및방법 |
RU2466068C1 (ru) * | 2011-04-08 | 2012-11-10 | Федеральное Государственное Унитарное Предприятие "Государственный научно-производственный ракетно-космический центр "ЦСКБ-Прогресс" (ФГУП "ГНПРКЦ "ЦСКБ-Прогресс") | Способ калибровки измерителей угловой скорости бесплатформенных инерциальных систем ориентации космических аппаратов и устройство его реализующее |
CN102466429A (zh) * | 2011-07-04 | 2012-05-23 | 北京科实医学图像技术研究所 | 宇宙火箭推力装置的改进方案 |
CN103543750B (zh) * | 2013-07-26 | 2016-03-02 | 西北工业大学 | 基于二次型规划的在轨服务航天器推力分配优化方法 |
RU2565426C2 (ru) * | 2014-03-12 | 2015-10-20 | Акционерное общество "Ракетно-космический центр "Прогресс" (АО "РКЦ "Прогресс") | Способ ориентации космических аппаратов и устройство его реализующее |
US10392136B2 (en) * | 2017-09-18 | 2019-08-27 | Raytheon Company | Offload adjustment for satellite image diversity |
CN108362292A (zh) * | 2018-02-13 | 2018-08-03 | 上海航天控制技术研究所 | 一种基于遗传算法的火星导航敏感器安装布局优化方法 |
CN111483617B (zh) * | 2020-04-09 | 2021-12-07 | 上海航天控制技术研究所 | 一种适用于火星探测的光照最优姿态机动路径规划方法 |
CN115771623A (zh) * | 2022-12-23 | 2023-03-10 | 上海航天控制技术研究所 | 一种用于卫星应急变轨的虚拟轨道构造方法 |
CN116674768B (zh) * | 2023-07-27 | 2023-09-29 | 北京航天驭星科技有限公司 | 电推进卫星的轨道机动方向估计方法、装置和存储介质 |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2373823A1 (fr) * | 1976-12-10 | 1978-07-07 | Matra | Procede et dispositif de commande d'attitude de vehicule spatial |
FR2583873B1 (fr) * | 1985-06-20 | 1987-09-11 | Matra | Procede et dispositif d'injection de satellite sur orbite geostationnaire avec stabilisation suivant les trois axes |
US4837699A (en) * | 1985-07-18 | 1989-06-06 | Hughes Aircraft Company | Method for controlling the spin axis attitude of a spinning spacecraft |
US4776540A (en) * | 1986-10-03 | 1988-10-11 | Communications Satellite Corporation | Method of orienting a synchronous satellite |
-
1988
- 1988-12-23 FR FR8817120A patent/FR2640933B1/fr not_active Expired - Fee Related
-
1989
- 1989-12-05 US US07/446,254 patent/US5064152A/en not_active Expired - Fee Related
- 1989-12-06 ES ES89403387T patent/ES2044189T3/es not_active Expired - Lifetime
- 1989-12-06 DE DE89403387T patent/DE68909389T2/de not_active Expired - Fee Related
- 1989-12-06 EP EP89403387A patent/EP0375496B1/fr not_active Expired - Lifetime
- 1989-12-08 CA CA002005025A patent/CA2005025A1/en not_active Abandoned
- 1989-12-20 JP JP1332454A patent/JPH02237897A/ja active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112537461A (zh) * | 2020-12-03 | 2021-03-23 | 北京航空航天大学 | 一种基于星载关联性健康基线卫星在轨实时监测方法 |
Also Published As
Publication number | Publication date |
---|---|
CA2005025A1 (en) | 1990-06-23 |
FR2640933A1 (es) | 1990-06-29 |
EP0375496B1 (fr) | 1993-09-22 |
DE68909389T2 (de) | 1994-02-03 |
US5064152A (en) | 1991-11-12 |
DE68909389D1 (de) | 1993-10-28 |
EP0375496A1 (fr) | 1990-06-27 |
FR2640933B1 (es) | 1991-04-12 |
JPH02237897A (ja) | 1990-09-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
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