WO2008054482A3 - Solar system positioning system - Google Patents

Solar system positioning system Download PDF

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Publication number
WO2008054482A3
WO2008054482A3 PCT/US2007/007407 US2007007407W WO2008054482A3 WO 2008054482 A3 WO2008054482 A3 WO 2008054482A3 US 2007007407 W US2007007407 W US 2007007407W WO 2008054482 A3 WO2008054482 A3 WO 2008054482A3
Authority
WO
WIPO (PCT)
Prior art keywords
transmitters
time data
receiver
solar
ephemeris
Prior art date
Application number
PCT/US2007/007407
Other languages
French (fr)
Other versions
WO2008054482A2 (en
Inventor
Arthur M Dula
Original Assignee
Arthur M Dula
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 Arthur M Dula filed Critical Arthur M Dula
Publication of WO2008054482A2 publication Critical patent/WO2008054482A2/en
Publication of WO2008054482A3 publication Critical patent/WO2008054482A3/en

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
    • B64G1/1014—Navigation satellites
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/24—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 specially adapted for cosmonautical navigation
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/02—Details of the space or ground control segments
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/03—Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers

Abstract

A trilateration positioning system comprising: a plurality of transmitters having known ephemerides that transmit dual frequency ephemeris and time data wherein at least one of said transmitters is beyond earth orbit; a plurality of transmitter clocks providing time data to each of said transmitters; a receiver that receives said dual frequency ephemeris and time data from four or more of said transmitters and uses trilateration to determine the location of said receiver; and a receiver clock providing time data to said receiver.
PCT/US2007/007407 2006-03-24 2007-03-26 Solar system positioning system WO2008054482A2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US74376506P 2006-03-24 2006-03-24
US60/743,765 2006-03-24

Publications (2)

Publication Number Publication Date
WO2008054482A2 WO2008054482A2 (en) 2008-05-08
WO2008054482A3 true WO2008054482A3 (en) 2008-08-28

Family

ID=39344787

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2007/007407 WO2008054482A2 (en) 2006-03-24 2007-03-26 Solar system positioning system

Country Status (1)

Country Link
WO (1) WO2008054482A2 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101308024B (en) * 2008-07-03 2010-10-13 上海交通大学 Orbit movement target parameter estimation system based on transient relative model
CN103591948B (en) * 2013-10-16 2014-11-19 北京控制工程研究所 Initial value synchronization method for improving landing navigation accuracy
CN104374403B (en) * 2014-10-28 2017-05-03 上海卫星工程研究所 Ground testing method of astronomical velocity-measuring autonomous navigation system by utilizing relative movement of celestial bodies
RU2627961C2 (en) * 2016-01-27 2017-08-14 Федеральное государственное казенное военное образовательное учреждение высшего образования "Военно-космическая академия имени А.Ф. Можайского" Министерства обороны Российской Федерации Method of determining location of meteor body
CN106767845B (en) * 2017-02-20 2019-09-24 中国人民解放军国防科学技术大学 Spacecraft air navigation aid based on the high rail of the earth-ground moon libration point Heterogeneous constellation
CN110686684B (en) * 2019-11-22 2021-09-24 北京理工大学 Optical collaborative orbit determination method for small celestial body surrounding detector

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06308262A (en) * 1993-04-27 1994-11-04 Mitsubishi Electric Corp Time synchronizing device for spacecraft
KR19990048901A (en) * 1997-12-11 1999-07-05 김영환 Positioning system of space vehicle using earth station transmission information
US6508438B2 (en) * 1999-08-13 2003-01-21 The Boeing Company Spacecraft orbit control using orbit position feedback
JP2003098246A (en) * 2001-09-26 2003-04-03 Mitsubishi Electric Corp Method of determining orbits of spacecraft group under formation navigation, and system therefor

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06308262A (en) * 1993-04-27 1994-11-04 Mitsubishi Electric Corp Time synchronizing device for spacecraft
KR19990048901A (en) * 1997-12-11 1999-07-05 김영환 Positioning system of space vehicle using earth station transmission information
US6508438B2 (en) * 1999-08-13 2003-01-21 The Boeing Company Spacecraft orbit control using orbit position feedback
JP2003098246A (en) * 2001-09-26 2003-04-03 Mitsubishi Electric Corp Method of determining orbits of spacecraft group under formation navigation, and system therefor

Also Published As

Publication number Publication date
WO2008054482A2 (en) 2008-05-08

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