IN2014DN03086A - - Google Patents
Info
- Publication number
- IN2014DN03086A IN2014DN03086A IN3086DEN2014A IN2014DN03086A IN 2014DN03086 A IN2014DN03086 A IN 2014DN03086A IN 3086DEN2014 A IN3086DEN2014 A IN 3086DEN2014A IN 2014DN03086 A IN2014DN03086 A IN 2014DN03086A
- Authority
- IN
- India
Links
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
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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
- B64G1/26—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
- B64G1/242—Orbits and trajectories
-
- 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
- B64G1/283—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using reaction wheels
-
- 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
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/407—Solar sailing
-
- 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
- B64G1/42—Arrangements or adaptations of power supply systems
- B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
- B64G1/443—Photovoltaic cell arrays
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Radar, Positioning & Navigation (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1102835A FR2980176A1 (en) | 2011-09-19 | 2011-09-19 | SATELLITE ATTITUDE CONTROL METHOD AND ATTITUDE CONTROL SATELLITE |
PCT/EP2012/068454 WO2013041575A1 (en) | 2011-09-19 | 2012-09-19 | Method of controlling the attitude of a satellite and an attitude-controlled satellite |
Publications (1)
Publication Number | Publication Date |
---|---|
IN2014DN03086A true IN2014DN03086A (en) | 2015-05-15 |
Family
ID=46875835
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IN3086DEN2014 IN2014DN03086A (en) | 2011-09-19 | 2014-04-17 |
Country Status (6)
Country | Link |
---|---|
US (1) | US9027887B2 (en) |
EP (1) | EP2758311B1 (en) |
CN (1) | CN103917451B (en) |
FR (1) | FR2980176A1 (en) |
IN (1) | IN2014DN03086A (en) |
WO (1) | WO2013041575A1 (en) |
Families Citing this family (45)
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CN103863578B (en) * | 2013-07-12 | 2016-03-30 | 北京航空航天大学 | Mars landing device jet thrust device and control moment gyroscope combined control system |
FR3013685B1 (en) * | 2013-11-25 | 2017-05-19 | Astrium Sas | METHOD AND DEVICE FOR CONTROLLING A SUN ACQUISITION PHASE BY A SPATIAL DEVICE |
WO2016022579A2 (en) * | 2014-08-05 | 2016-02-11 | Massachusetts Institute Of Technology | Design of a free-space optical communication module for small satellites |
CN104179983A (en) * | 2014-08-19 | 2014-12-03 | 江苏中寰卫星导航通信有限公司 | Maze type satellite rotary seal mechanism |
WO2016030890A1 (en) | 2014-08-26 | 2016-03-03 | Effective Space Solutions Ltd | Docking system and method for satellites |
FR3026858B1 (en) * | 2014-10-02 | 2016-12-09 | Airbus Defence & Space Sas | METHOD FOR CONTROLLING ATTITUDE OF SATELLITE IN SURVIVAL MODE, ADAPTED SATELLITE AND METHOD FOR REMOTELY CONTROLLING SATELLITE OF SATELLITE |
CN104477413B (en) * | 2014-11-06 | 2016-06-01 | 中国空间技术研究院 | A kind of based on electric thruster carry out position guarantor and momenttum wheel unloading combination control method |
US11009297B2 (en) * | 2015-04-15 | 2021-05-18 | Worldvu Satellites Limited | Fluidicially coupled heat pipes and method therefor |
JP6586658B2 (en) * | 2015-05-12 | 2019-10-09 | 国立研究開発法人宇宙航空研究開発機構 | Torque generation system, spacecraft attitude control system, spacecraft relative position / speed control system |
US9764859B2 (en) * | 2015-06-29 | 2017-09-19 | The Boeing Company | Efficient stationkeeping design for mixed fuel systems |
US9963249B2 (en) * | 2015-06-29 | 2018-05-08 | The Boeing Company | Efficient stationkeeping design for mixed fuel systems in response to a failure of an electric thruster |
WO2017025778A1 (en) * | 2015-08-12 | 2017-02-16 | Uab "Pazangus Pozicionavimo Sprendimai" | Satellites attitude control system |
US10183764B1 (en) * | 2015-11-12 | 2019-01-22 | Space Systems/Loral, Llc | High capacity spacecraft |
US10005568B2 (en) * | 2015-11-13 | 2018-06-26 | The Boeing Company | Energy efficient satellite maneuvering |
CN105607478B (en) * | 2016-01-21 | 2017-07-07 | 北京理工大学 | Geostationary orbit spacecraft electric propulsion transfer orbit control method |
US9963248B2 (en) * | 2016-02-04 | 2018-05-08 | The Boeing Company | Spin stabilization of a spacecraft for an orbit maneuver |
US10144531B2 (en) | 2016-02-04 | 2018-12-04 | The Boeing Company | Reorientation of a spinning spacecraft using gimbaled electric thrusters |
FR3047813B1 (en) * | 2016-02-16 | 2019-11-08 | Airbus Defence And Space Sas | METHOD FOR CONTROLLING SATELLITE ATTITUDE GUIDANCE, SATELLITE, SATELLITE PLURALITIES AND ASSOCIATED COMPUTER PROGRAM |
WO2017218696A1 (en) * | 2016-06-14 | 2017-12-21 | Blomquist Richard | Spacecraft and control method |
CN106005483B (en) * | 2016-07-06 | 2018-07-24 | 西北工业大学 | A kind of active attitude control method of modular mobile phone star |
CN106628261B (en) * | 2016-10-20 | 2018-11-20 | 上海航天控制技术研究所 | It is a kind of electricity pushing protect during the high stability attitude control method of satellite high-precision |
EP3330189B1 (en) * | 2016-12-05 | 2019-06-19 | Airbus Defence and Space GmbH | Pointing mechanism for use in an electric propulsion system of a spacecraft |
US9663252B1 (en) * | 2016-12-07 | 2017-05-30 | Beihang University | Method for attitude controlling based on finite time friction estimation for flexible spacecraft |
US10625882B2 (en) * | 2017-03-06 | 2020-04-21 | Effective Space Solutions Ltd. | Service satellite for providing in-orbit services using variable thruster control |
US10435183B1 (en) | 2017-04-14 | 2019-10-08 | Space Systems/Loral, Llc | Deployable propulsion module for spacecraft |
CN107323690B (en) * | 2017-05-17 | 2020-03-06 | 上海卫星工程研究所 | Satellite large-angle momentum compensation synchronism design method |
CN107264838B (en) * | 2017-06-21 | 2019-05-21 | 西北工业大学深圳研究院 | A kind of chip satellite and its attitude control method based on electroactive polymer |
KR101877414B1 (en) * | 2017-09-22 | 2018-07-12 | 한국항공우주연구원 | Control method of angular momentum of a satellite |
CN107472396B (en) * | 2017-09-26 | 2021-04-27 | 北京航空航天大学 | Quadruped robot capable of realizing air posture adjustment |
WO2019191294A1 (en) * | 2018-03-27 | 2019-10-03 | Massachusetts Institute Of Technology | Methods and apparatus for in-situ measurements of atmospheric density |
CN108820257B (en) * | 2018-06-25 | 2020-05-29 | 上海卫星工程研究所 | Moment checking method of stepping motor mechanism for satellite |
CN109747867B (en) * | 2018-12-12 | 2022-03-04 | 兰州空间技术物理研究所 | Vector adjustment mechanism for electric thruster |
CN109703783B (en) * | 2018-12-29 | 2022-06-14 | 西北工业大学 | Satellite attitude self-rescue device and satellite with same |
FR3093998B1 (en) * | 2019-03-20 | 2021-09-10 | Airbus Defence & Space Sas | Method for controlling the attitude of a satellite in survival mode without a priori knowledge of the local time of the orbit of the satellite |
FR3094479B1 (en) * | 2019-03-25 | 2021-08-27 | Airbus Defence & Space Sas | Device and method for determining the attitude of a satellite equipped with gyroscopic actuators, and a satellite carrying such a device |
US11230384B2 (en) | 2019-04-23 | 2022-01-25 | Joby Aero, Inc. | Vehicle cabin thermal management system and method |
CN110576983B (en) * | 2019-08-26 | 2021-03-16 | 上海航天控制技术研究所 | Attitude determination method in track transfer process |
EP4112482A4 (en) * | 2020-02-26 | 2023-04-05 | Mitsubishi Electric Corporation | Orbital attitude control device, satellite, orbital attitude control method, and program |
FR3110144A1 (en) * | 2020-05-12 | 2021-11-19 | Airbus Defence And Space Sas | Method of orbit control and desaturation of a satellite by means of a single articulated arm carrying a propulsion unit |
CN115836493A (en) * | 2020-07-10 | 2023-03-21 | 星网有限责任公司 | Data transmission system and method for low earth orbit satellite and very low earth orbit satellite communications |
JP7426714B2 (en) * | 2020-07-15 | 2024-02-02 | 国立研究開発法人宇宙航空研究開発機構 | Optical devices and spacecraft using them |
CN113173271A (en) * | 2021-05-28 | 2021-07-27 | 重庆协点通讯技术有限公司 | Star chain receiving arrangement convenient to adjust |
CN115297152B (en) * | 2022-10-08 | 2022-12-27 | 中科星图测控技术(合肥)有限公司 | Satellite-borne auxiliary measurement and control device and method |
CN117485595B (en) * | 2023-11-21 | 2024-04-05 | 北京易动宇航科技有限公司 | Energy management method for electric propulsion system |
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CN101934863B (en) * | 2010-09-29 | 2013-04-03 | 哈尔滨工业大学 | Satellite posture all-round controlling method based on magnetic moment device and flywheel |
FR2970701B1 (en) * | 2011-01-25 | 2015-04-17 | Astrium Sas | SATELLITE ATTITUDE CONTROL DEVICE AND METHOD FOR CONTROLLING A SATELLITE EMBEDDING SAID DEVICE |
US8868263B2 (en) * | 2011-05-25 | 2014-10-21 | Space Systems/Loral, Llc | Spacecraft momentum management using solar array |
-
2011
- 2011-09-19 FR FR1102835A patent/FR2980176A1/en active Pending
-
2012
- 2012-09-19 WO PCT/EP2012/068454 patent/WO2013041575A1/en active Application Filing
- 2012-09-19 CN CN201280054916.4A patent/CN103917451B/en active Active
- 2012-09-19 US US14/345,515 patent/US9027887B2/en active Active
- 2012-09-19 EP EP12759743.3A patent/EP2758311B1/en active Active
-
2014
- 2014-04-17 IN IN3086DEN2014 patent/IN2014DN03086A/en unknown
Also Published As
Publication number | Publication date |
---|---|
CN103917451A (en) | 2014-07-09 |
US9027887B2 (en) | 2015-05-12 |
US20150001345A1 (en) | 2015-01-01 |
CN103917451B (en) | 2016-03-23 |
FR2980176A1 (en) | 2013-03-22 |
WO2013041575A1 (en) | 2013-03-28 |
EP2758311B1 (en) | 2017-02-15 |
EP2758311A1 (en) | 2014-07-30 |