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Title: US6556808: Fixed ground track satellite constellation and user terminal
[ Derwent Title ]


Country: US United States of America

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9 pages

 
Inventor: De La Chapelle, Michael; Bellevue, WA
Hargraves, Charles R.; Renton, WA
Olcott, Timothy A.; Maple Valley, WA
Raubenstine, Terry L.; Seattle, WA
Clue, Ira J.; Renton, WA
Barclay, Charles C.; Renton, WA

Assignee: The Boeing Company, Chicago, IL
other patents from BOEING COMPANY (70060) (approx. 4,331)
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Published / Filed: 2003-04-29 / 1998-12-30

Application Number: US1998000224561

IPC Code: Advanced: H04B 7/195;
Core: more...
IPC-7: H04B 7/185;

ECLA Code: H04B7/195;

U.S. Class: Current: 455/012.1; 244/158.4; 342/354; 455/013.1;
Original: 455/012.1; 244/158.R; 455/013.1; 342/354;

Field of Search: 455/12.1,13.1,13.2,456,13.3 244/158 R,164 342/354,358,450

Priority Number:
1998-12-30  US1998000224561

Abstract: A satellite communication system includes a constellation of non-geostationary orbiting satellites following a fixed ground track on the earth, and ground terminals having substantially continuous visibility to at least one of the satellites in a single ground track. Each of the satellites in the constellation follows a single substantially linear track across the sky when observed from the earth. In a preferred embodiment, the system can also include ground terminals which have an antenna with a single axis of scanning motion. In this embodiment, satellites have repeating ground tracks wherein a satellite completes n orbital revolutions each time the earth rotates through 360 degrees, wherein n is an integer between 2 and 15, inclusive.

Attorney, Agent or Firm: Nelson, Lawrence W. ;

Primary / Asst. Examiners: Maung, Nay; Contee, Joy K.

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Designated Country: AE AL AM AP AT AZ BA BB BG BR BY CA CH CN CU CZ DE DK EA EE EP ES FI GB GD GE GH GM HR HU ID IL IN IS JP KE KG KP KR 

Family: Show 3 known family members

First Claim:
Show all 11 claims
What is claimed is:     1. A constellation of satellites comprising:
  • a plurality of non-geostationary low earth orbit satellites in circular orbit around earth; and
  • a substantially continuous ground track provided by one of said plurality of satellites following one another;
  • wherein each of said plurality of satellites has an even number of revolutions around the earth per day; and
  • wherein said ground track is substantially stationary with respect to a given position on the earth's surface.


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U.S. References: Go to Result Set: All U.S. references   |  No patents reference this one   |   Backward references (23)   |   Citation Link

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Patent  Pub.Date  Inventor Assignee   Title
Buy PDF- 9pp US4809935  1989-03 Draim  Analytic Services, Inc. Satellite continuous coverage constellations
Buy PDF- 9pp US5075682  1991-12 Dehnert   Antenna mount and method for tracking a satellite moving in an inclined orbit
Buy PDF- 12pp US5119225  1992-06 Grant et al.  British Aerospace Public Limited Company Multiple access communication system
Buy PDF- 37pp US5551624  1996-09 Horstein et al.  TRW Inc. Medium-earth-altitude satellite-based cellular telecommunications
Buy PDF- 15pp US5579536  1996-11 Stackman et al.  Motorola, Inc. Method and apparatus for establishing communication links between non-stationary communication units
Buy PDF- 22pp US5582367  1996-12 Castiel et al.  Mobile Communications Holdings, Inc. Elliptical orbit satellite, system, and deployment with controllable coverage characteristics
Buy PDF- 24pp US5621415  1997-04 Tuck  Teledesic Corporation Linear cell satellite system
Buy PDF- 24pp US5722042  1998-02 Kimura et al.  ATR Optical and Radio Communications Research Laboratories Satellite communication system having double-layered earth orbit satellite constellation with two different altitudes
Buy PDF- 7pp US5729240  1998-03 Bourgeois  Alcatel Telspace Method of controlling a non-geostationary satellite antenna positioner
Buy PDF- 17pp US5765098  1998-06 Bella  Agence Spatiale Europeenne Method and system for transmitting radio signals between a fixed terrestrial station and user mobile terminals via a network of satellites
Buy PDF- 7pp US5797083  1998-08 Anderson  Hughes Electronics Corporation Self-aligning satellite receiver antenna
Buy PDF- 37pp US5867783  1999-02 Horstein et al.  TRW Inc. Medium-earth-altitute satellite-based cellular telecommunications
Buy PDF- 14pp US5931417  1999-08 Castiel  Mobile Communications Holdings, Inc. Non-geostationary orbit satellite constellation for continuous coverage of northern latitudes above 25° and its extension to global coverage tailored to the distribution of populated land masses on earth
Buy PDF- 17pp US5978653  1999-11 Taylor et al.  Motorola, Inc. Method and apparatus for providing additional resources in a satellite communication system
Buy PDF- 11pp US6019318  2000-02 Cellier et al.  Hugehs Electronics Corporation Coordinatable system of inclined geosynchronous satellite orbits
Buy PDF- 24pp US6078284  2000-06 Levanon  QUALCOMM Incorporated Passive position determination using two low-earth orbit satellites
Buy PDF- 14pp US6085090  2000-07 Yee et al.  Motorola, Inc. Autonomous interrogatable information and position device
Buy PDF- 9pp US6088571  2000-07 Kane et al.  Motorola, Inc. Method and apparatus for multi-constellation satellite broadcast with error correction
Buy PDF- 11pp US6097929  2000-08 Hassall et al.  Telogy Networks, Inc. Method and system for monitoring and controlling a single channel per carrier satellite link between two remote earth stations
Buy PDF- 29pp US6102335  2000-08 Castiel et al.  Mobile Communications Holdings, Inc. Elliptical orbit satellite, system, and deployment with controllable coverage characteristics
Buy PDF- 14pp US6122596  2000-09 Castiel  Mobile Communications Holdings, Inc. Non-geostationary orbit satelite constellation for continuous preferential coverage of northern latitudes
Buy PDF- 14pp US6126116  2000-10 Cellier  Hughes Electronics Corporation Coordinatable system of inclined eccentric geosynchronous orbits
Buy PDF- 18pp US6198907  2001-03 Torkington et al.  Motorola, Inc. Satellite communications systems using satellites in a zero-drift constellation
       
Foreign References:
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PDF
Publication Date IPC Code Assignee   Title
Buy PDF- 8pp EP0588697 1994-03  H04B 7/185 FRANCE TELECOM Telecommunication network with low altitude orbiting satellite constellation and high latitude earth station for orbit interconnection 
Buy PDF- 34pp EP0601293 1994-06  G01S 5/12 MOTOROLA INC Intelligent position tracking 
Buy PDF- 34pp EP0601293 1994-06  G01S 5/12 MOTOROLA INC Intelligent position tracking 
Buy PDF- 11pp EP0836290 1998-04  B64G 1/00 NORTEL NETWORKS CORPORATION Satellite communication method using satellites on substantially circular orbit, inclined to the equatorial plane with period matching the earth period 
Buy PDF FR2685833 1993-07  B64G 1/00 AGENCE SPATIALE EUROPEENNE RESEAU DE SATELLITES DE COMMUNICATION. 


Other Abstract Info: DERABS G2000-586917

Other References:
  • Wang, Chia-Jiu: "Structural Properties of a Low Earth Orbit Satellite Constellation--The Walker Delta Network"--Proceedings of the Annual Military Communications Conference (MILCOM), US, New York, IEEE, vol. CONF. 12, 1993, pp. 968-972, XP000410896, p. 968, right-hand column, line 21--p. 969, left-hand column, line 5.


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