WO2015160416A3 - Communication satellite system - Google Patents
Communication satellite system Download PDFInfo
- Publication number
- WO2015160416A3 WO2015160416A3 PCT/US2015/013941 US2015013941W WO2015160416A3 WO 2015160416 A3 WO2015160416 A3 WO 2015160416A3 US 2015013941 W US2015013941 W US 2015013941W WO 2015160416 A3 WO2015160416 A3 WO 2015160416A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- orbit
- satellite
- poles
- satellite system
- satellites
- Prior art date
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
- B64G1/242—Orbits and trajectories
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
- B64G1/1007—Communications satellites
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
- B64G1/1085—Swarms and constellations
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Astronomy & Astrophysics (AREA)
- General Physics & Mathematics (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Radar, Positioning & Navigation (AREA)
- Radio Relay Systems (AREA)
Abstract
A method of providing satellite coverage to the Northern and Southern Polar Regions includes launching multiple satellites into orbit with each satellite's orbit moving in the direction of one of the poles. The satellites are sequentially launched into orbit at differing values of the argument of perigee (ω). Each launch is spaced apart in time by a predetermined amount. Each satellite has an elliptical orbit and an orbital inclination that causes an orbital drift rate such that, over time, the apogee of the elliptical orbit moves in the direction of one of the poles at a predetermined rate.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201461934078P | 2014-01-31 | 2014-01-31 | |
US61/934,078 | 2014-01-31 |
Publications (3)
Publication Number | Publication Date |
---|---|
WO2015160416A2 WO2015160416A2 (en) | 2015-10-22 |
WO2015160416A3 true WO2015160416A3 (en) | 2015-12-03 |
WO2015160416A9 WO2015160416A9 (en) | 2016-01-21 |
Family
ID=54324691
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2015/013941 WO2015160416A2 (en) | 2014-01-31 | 2015-01-30 | Communication satellite system |
Country Status (1)
Country | Link |
---|---|
WO (1) | WO2015160416A2 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3380400B1 (en) * | 2015-11-27 | 2021-02-17 | Telesat Canada | Satellite system and method for global coverage |
US10364051B1 (en) | 2016-11-15 | 2019-07-30 | Space Systems/Loral, Llc | Efficient stationkeeping strategy for the three apogee (TAP) orbit |
CN116430725B (en) * | 2023-03-24 | 2024-03-29 | 中国西安卫星测控中心 | GEO satellite east-west control quantity optimization selection method |
CN116151052B (en) * | 2023-04-24 | 2023-07-04 | 中国人民解放军32035部队 | Method and device for heavily orbit-changing losing recapture of certain satellite and electronic equipment |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3215365A (en) * | 1963-04-30 | 1965-11-02 | Wyatt Theodore | Spacecraft propulsion concept |
US20030132350A1 (en) * | 1999-07-09 | 2003-07-17 | David Goldstein | Orbit transfer vehicle with support services |
US20050178918A1 (en) * | 1998-05-20 | 2005-08-18 | Toshihide Maeda | Communication system, communication receiving device and communication terminal in the system |
US20070135040A1 (en) * | 2005-12-12 | 2007-06-14 | Draim John E | Methods for effecting seamless handover and enhancing capacity in elliptical orbit satellite communications systems |
US7720604B1 (en) * | 2005-06-01 | 2010-05-18 | Lockheed Martin Corporation | Stationkeeping optimization for inclined elliptical satellite orbit constellations |
-
2015
- 2015-01-30 WO PCT/US2015/013941 patent/WO2015160416A2/en active Application Filing
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3215365A (en) * | 1963-04-30 | 1965-11-02 | Wyatt Theodore | Spacecraft propulsion concept |
US20050178918A1 (en) * | 1998-05-20 | 2005-08-18 | Toshihide Maeda | Communication system, communication receiving device and communication terminal in the system |
US20030132350A1 (en) * | 1999-07-09 | 2003-07-17 | David Goldstein | Orbit transfer vehicle with support services |
US7720604B1 (en) * | 2005-06-01 | 2010-05-18 | Lockheed Martin Corporation | Stationkeeping optimization for inclined elliptical satellite orbit constellations |
US20070135040A1 (en) * | 2005-12-12 | 2007-06-14 | Draim John E | Methods for effecting seamless handover and enhancing capacity in elliptical orbit satellite communications systems |
Also Published As
Publication number | Publication date |
---|---|
WO2015160416A2 (en) | 2015-10-22 |
WO2015160416A9 (en) | 2016-01-21 |
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