CA2165875A1 - Intersatellite communications systems - Google Patents
Intersatellite communications systemsInfo
- Publication number
- CA2165875A1 CA2165875A1 CA002165875A CA2165875A CA2165875A1 CA 2165875 A1 CA2165875 A1 CA 2165875A1 CA 002165875 A CA002165875 A CA 002165875A CA 2165875 A CA2165875 A CA 2165875A CA 2165875 A1 CA2165875 A1 CA 2165875A1
- Authority
- CA
- Canada
- Prior art keywords
- satellite
- satellites
- channel
- incoming
- beams
- 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.)
- Granted
Links
Classifications
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04B—TRANSMISSION
- H04B7/00—Radio transmission systems, i.e. using radiation field
- H04B7/14—Relay systems
- H04B7/15—Active relay systems
- H04B7/185—Space-based or airborne stations; Stations for satellite systems
- H04B7/18521—Systems of inter linked satellites, i.e. inter satellite service
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Astronomy & Astrophysics (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Physics & Mathematics (AREA)
- Computer Networks & Wireless Communication (AREA)
- Signal Processing (AREA)
- Radio Relay Systems (AREA)
Abstract
A multibeam communications satellite has direct links with at least one other satellite.
The satellite's repeater operates in the bent-pipe mode and can provide service to users independent of signal content, format and protocol. Each incoming electromagnetic (radio) beam received by the satellite contains at least one channel of information, and each channel is divisible into subchannels. Naturally, each subchannel is of a bandwidth which is less than the bandwidth of the channel from which the subchannel was derived.
The other satellite has outgoing beams that complement the first satellites incoming beams. Generally, both satellites have processors on board designed to interbeam-switch at the subchannel level. (However, a description is given also of an instance where one or the other satellites may not have subchannelizing capability and limited use may be made of the invention). The satellites are linked by an intersatellite link carrying information on a channel consisting of subchannels constituted from several incoming channels. Therefore, an outgoing beam from the second satellite can contain a channel having information combined from several incoming channels to the first satellite and the channel information on any incoming electromagnetic (radio) beam can be delivered at the subchannel level to several output beams from the second satellite. The system can operate in a broadcast mode whereby information at the subchannel level can be distributed simultaneously (i.e. in parallel) to several outgoing electromagnetic (radio) beams. The intersatellite link is treated as any other beam (incoming or outgoing, as the case may be), although its operating wavelength may be different from the operating wavelengths of the beams having terrestrial origin or destination. For example, the intersatellite link could be at microwave, optical or some other suitable frequency. The basic concept may be extended to a system supporting multiple intersatellite links, e.g.
links in both directions between the two satellites or, in some circumstances, among a constellation of more than two satellites.
The satellite's repeater operates in the bent-pipe mode and can provide service to users independent of signal content, format and protocol. Each incoming electromagnetic (radio) beam received by the satellite contains at least one channel of information, and each channel is divisible into subchannels. Naturally, each subchannel is of a bandwidth which is less than the bandwidth of the channel from which the subchannel was derived.
The other satellite has outgoing beams that complement the first satellites incoming beams. Generally, both satellites have processors on board designed to interbeam-switch at the subchannel level. (However, a description is given also of an instance where one or the other satellites may not have subchannelizing capability and limited use may be made of the invention). The satellites are linked by an intersatellite link carrying information on a channel consisting of subchannels constituted from several incoming channels. Therefore, an outgoing beam from the second satellite can contain a channel having information combined from several incoming channels to the first satellite and the channel information on any incoming electromagnetic (radio) beam can be delivered at the subchannel level to several output beams from the second satellite. The system can operate in a broadcast mode whereby information at the subchannel level can be distributed simultaneously (i.e. in parallel) to several outgoing electromagnetic (radio) beams. The intersatellite link is treated as any other beam (incoming or outgoing, as the case may be), although its operating wavelength may be different from the operating wavelengths of the beams having terrestrial origin or destination. For example, the intersatellite link could be at microwave, optical or some other suitable frequency. The basic concept may be extended to a system supporting multiple intersatellite links, e.g.
links in both directions between the two satellites or, in some circumstances, among a constellation of more than two satellites.
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA002165875A CA2165875C (en) | 1995-12-21 | 1995-12-21 | Intersatellite communications systems |
US08/715,065 US5825325A (en) | 1995-12-21 | 1996-09-17 | Intersatellite communications systems |
EP19960119806 EP0780998B1 (en) | 1995-12-21 | 1996-12-10 | Intersatellite communication system with switching at subchannel level using bent-pipe architecture |
DE69627284T DE69627284T2 (en) | 1995-12-21 | 1996-12-10 | Intersatellite communication arrangement with subchannel switching and bent pipe architecture |
NO965313A NO965313L (en) | 1995-12-21 | 1996-12-12 | Inter Satellite |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA002165875A CA2165875C (en) | 1995-12-21 | 1995-12-21 | Intersatellite communications systems |
Publications (2)
Publication Number | Publication Date |
---|---|
CA2165875A1 true CA2165875A1 (en) | 1997-06-22 |
CA2165875C CA2165875C (en) | 2001-03-13 |
Family
ID=4157214
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA002165875A Expired - Fee Related CA2165875C (en) | 1995-12-21 | 1995-12-21 | Intersatellite communications systems |
Country Status (2)
Country | Link |
---|---|
US (1) | US5825325A (en) |
CA (1) | CA2165875C (en) |
Families Citing this family (36)
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US6708029B2 (en) | 1997-06-02 | 2004-03-16 | Hughes Electronics Corporation | Broadband communication system for mobile users in a satellite-based network |
US6125261A (en) * | 1997-06-02 | 2000-09-26 | Hughes Electronics Corporation | Method and system for communicating high rate data in a satellite-based communications network |
US6032041A (en) * | 1997-06-02 | 2000-02-29 | Hughes Electronics Corporation | Method and system for providing wideband communications to mobile users in a satellite-based network |
US6175719B1 (en) * | 1997-06-25 | 2001-01-16 | Hughes Electronics Corporation | Multi-spot-beam satellite system with broadcast and surge capacity capability |
US6282179B1 (en) * | 1997-10-17 | 2001-08-28 | At&T Corp. | Method and system for reducing multipath fading in bent-pipe satellite communications systems |
AU2456899A (en) * | 1998-02-18 | 1999-09-06 | Viasat, Inc. | Method for improving inter-beam capacity switching for multiple spot beam satellite systems |
FR2777721B1 (en) * | 1998-04-16 | 2000-12-15 | Alsthom Cge Alkatel | COMMUNICATION METHOD BETWEEN LAND STATIONS USING SATELLITE CONSTELLATION |
US7027769B1 (en) | 2000-03-31 | 2006-04-11 | The Directv Group, Inc. | GEO stationary communications system with minimal delay |
EP1148661A3 (en) * | 2000-04-21 | 2003-10-29 | Lockheed Martin Corporation | Geostationary satellite system with satellite clusters having intra-cluster local area networks and inter-cluster wide area network |
US7058140B2 (en) * | 2000-06-16 | 2006-06-06 | Smart Kevin J | Sliding-window multi-carrier frequency division multiplexing system |
US6829479B1 (en) * | 2000-07-14 | 2004-12-07 | The Directv Group. Inc. | Fixed wireless back haul for mobile communications using stratospheric platforms |
US6859652B2 (en) | 2000-08-02 | 2005-02-22 | Mobile Satellite Ventures, Lp | Integrated or autonomous system and method of satellite-terrestrial frequency reuse using signal attenuation and/or blockage, dynamic assignment of frequencies and/or hysteresis |
US6895217B1 (en) | 2000-08-21 | 2005-05-17 | The Directv Group, Inc. | Stratospheric-based communication system for mobile users having adaptive interference rejection |
US6868269B1 (en) | 2000-08-28 | 2005-03-15 | The Directv Group, Inc. | Integrating coverage areas of multiple transponder platforms |
US7792488B2 (en) | 2000-12-04 | 2010-09-07 | Atc Technologies, Llc | Systems and methods for transmitting electromagnetic energy over a wireless channel having sufficiently weak measured signal strength |
US7019882B1 (en) | 2002-03-21 | 2006-03-28 | Lockheed Martin Corporation | Generation of M-ary digital signaling constellations directly at lightwave frequencies |
US7177592B2 (en) * | 2003-05-30 | 2007-02-13 | The Boeing Company | Wireless communication system with split spot beam payload |
KR100579127B1 (en) * | 2003-11-19 | 2006-05-12 | 한국전자통신연구원 | Satellite transponder switch control apparatus and method for multibeam communication |
US7460830B2 (en) * | 2003-12-29 | 2008-12-02 | Peersat, Llc. | Inter-satellite crosslink communications system, apparatus, method and computer program product |
US7738837B2 (en) * | 2005-02-22 | 2010-06-15 | Atc Technologies, Llc | Satellites using inter-satellite links to create indirect feeder link paths |
US20090295628A1 (en) * | 2006-09-26 | 2009-12-03 | Viasat, Inc. | Satellite System Optimization |
US8538323B2 (en) * | 2006-09-26 | 2013-09-17 | Viasat, Inc. | Satellite architecture |
EP2645596B2 (en) | 2006-09-26 | 2020-02-12 | ViaSat, Inc. | Improved spot beam satellite systems |
CN101573892A (en) * | 2006-10-03 | 2009-11-04 | 维尔塞特公司 | Large packet concatenation in satellite communication system |
EP2092663A2 (en) * | 2006-10-03 | 2009-08-26 | ViaSat, Inc. | Upfront delayed concatenation in satellite communication system |
CN101573889B (en) * | 2006-10-03 | 2014-05-14 | 维尔塞特公司 | Web/bulk transfer preallocation of upstream resources in satellite communication system |
WO2008060759A2 (en) * | 2006-10-03 | 2008-05-22 | Viasat, Inc. | Map-trigger dump of packets in satellite communication system |
US7869759B2 (en) * | 2006-12-14 | 2011-01-11 | Viasat, Inc. | Satellite communication system and method with asymmetric feeder and service frequency bands |
US20100059294A1 (en) * | 2008-09-08 | 2010-03-11 | Apple Inc. | Bandwidth enhancement for a touch sensor panel |
FR2952451B1 (en) * | 2009-11-10 | 2011-12-23 | Thales Sa | DYNAMIC MANAGEMENT OF THE FREQUENCY ROUTING CAPABILITY OF A TRANSPARENT DIGITAL PROCESSOR |
FR2954634B1 (en) * | 2009-12-18 | 2012-02-24 | Thales Sa | SYSTEM FOR TRANSMITTING AND RECEIVING MULTI-SPOTS OF A SATELLITE AND SATELLITE COMPRISING SUCH A SYSTEM |
US9749037B2 (en) * | 2013-04-18 | 2017-08-29 | Mitsubishi Electric Corporation | Demultiplexing apparatus, multiplexing apparatus, and relay apparatus |
US9991944B2 (en) * | 2015-01-15 | 2018-06-05 | Hughes Network Systems, Llc | High altitude platform with multibeam coverage for aero-based terminals |
AU2016302616B2 (en) * | 2015-07-31 | 2020-06-25 | Viasat, Inc. | Flexible capacity satellite constellation |
EP3361651A1 (en) * | 2017-02-10 | 2018-08-15 | Airbus Defence and Space Limited | Ultra-low latency telecommunications system |
CN112968725B (en) * | 2019-12-13 | 2022-05-13 | 清华大学 | Satellite link switching method and device |
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DE1943735A1 (en) * | 1969-08-28 | 1971-03-11 | Licentia Gmbh | Directional radio system |
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US4425639A (en) * | 1981-01-12 | 1984-01-10 | Bell Telephone Laboratories, Incorporated | Satellite communications system with frequency channelized beams |
US4456988A (en) * | 1981-01-29 | 1984-06-26 | Kokusai Denshin Denwa Kabushiki Kaisha | Satellite repeater |
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FR2694855B1 (en) * | 1992-08-14 | 1994-09-30 | Alcatel Espace | Transparent switching device, in particular for the space domain, payload architectures using such a device, and methods of implementing the device and the architectures. |
US5396643A (en) * | 1992-08-24 | 1995-03-07 | Motorola, Inc. | Geographic-area selective low-earth satellite-based paging broadcast system and method |
US5394560A (en) * | 1992-09-30 | 1995-02-28 | Motorola, Inc. | Nationwide satellite message delivery system |
US5483664A (en) * | 1993-07-26 | 1996-01-09 | Motorola, Inc. | Cellular communications with scheduled handoffs |
US5499237A (en) * | 1995-03-23 | 1996-03-12 | Motorola, Inc. | Waste canceling packet routing system and method |
-
1995
- 1995-12-21 CA CA002165875A patent/CA2165875C/en not_active Expired - Fee Related
-
1996
- 1996-09-17 US US08/715,065 patent/US5825325A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US5825325A (en) | 1998-10-20 |
CA2165875C (en) | 2001-03-13 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
EEER | Examination request | ||
MKLA | Lapsed |