AU2002357912A8 - A highly elliptical orbit for communications satellites - Google Patents

A highly elliptical orbit for communications satellites

Info

Publication number
AU2002357912A8
AU2002357912A8 AU2002357912A AU2002357912A AU2002357912A8 AU 2002357912 A8 AU2002357912 A8 AU 2002357912A8 AU 2002357912 A AU2002357912 A AU 2002357912A AU 2002357912 A AU2002357912 A AU 2002357912A AU 2002357912 A8 AU2002357912 A8 AU 2002357912A8
Authority
AU
Australia
Prior art keywords
elliptical orbit
communications satellites
highly elliptical
highly
satellites
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.)
Abandoned
Application number
AU2002357912A
Other versions
AU2002357912A1 (en
Inventor
Paul Heinerscheid
Alan Kidd
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Global Radio SA
Original Assignee
Global Radio SA
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Global Radio SA filed Critical Global Radio SA
Publication of AU2002357912A1 publication Critical patent/AU2002357912A1/en
Publication of AU2002357912A8 publication Critical patent/AU2002357912A8/en
Abandoned legal-status Critical Current

Links

Classifications

    • 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
    • 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
    • B64G1/22—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
    • 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
    • H04B7/195—Non-synchronous stations

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Signal Processing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Radio Relay Systems (AREA)
AU2002357912A 2001-12-21 2002-12-20 A highly elliptical orbit for communications satellites Abandoned AU2002357912A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US34183801P 2001-12-21 2001-12-21
US60/341,838 2001-12-21
PCT/US2002/040662 WO2003061141A2 (en) 2001-12-21 2002-12-20 A highly elliptical orbit for communications satellites

Publications (2)

Publication Number Publication Date
AU2002357912A1 AU2002357912A1 (en) 2003-07-30
AU2002357912A8 true AU2002357912A8 (en) 2003-07-30

Family

ID=23339231

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2002357912A Abandoned AU2002357912A1 (en) 2001-12-21 2002-12-20 A highly elliptical orbit for communications satellites

Country Status (3)

Country Link
EP (1) EP1512233A2 (en)
AU (1) AU2002357912A1 (en)
WO (1) WO2003061141A2 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7669803B2 (en) 2004-12-07 2010-03-02 Lockheed Martin Corporation Optimized land mobile satellite system for north american coverage
US7624948B2 (en) 2004-12-07 2009-12-01 Lockheed Martin Corporation Optimized land mobile satellite configuration and steering method
FR2918827B1 (en) * 2007-07-10 2009-10-16 Astrium Sas SYSTEM FOR POSITIONING A TERRESTRIAL USER.
CA2716174C (en) * 2010-10-01 2019-11-26 Telesat Canada Satellite system
US9365299B2 (en) 2014-06-09 2016-06-14 Space Systems/Loral, Llc Highly inclined elliptical orbit launch and orbit acquisition techniques
US9550585B2 (en) 2014-06-09 2017-01-24 Space Systems/Loral, Llc Highly inclined elliptical orbit de-orbit techniques

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5439190A (en) * 1991-04-22 1995-08-08 Trw Inc. Medium-earth-altitude satellite-based cellular telecommunications
US5525999A (en) * 1994-11-28 1996-06-11 Motorola, Inc. Multi-receiver master control station for differential GPS and method

Also Published As

Publication number Publication date
AU2002357912A1 (en) 2003-07-30
EP1512233A2 (en) 2005-03-09
WO2003061141A2 (en) 2003-07-24
WO2003061141A3 (en) 2003-12-18

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Legal Events

Date Code Title Description
MK6 Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase