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Autonomous navigation using lunar beaconsThe concept of using lunar beacon signal transmission for on-board navigation for earth satellites and near-earth spacecraft is described. The system would require powerful transmitters on the earth-side of the moon's surface and black box receivers with antennae and microprocessors placed on board spacecraft for autonomous navigation. Spacecraft navigation requires three position and three velocity elements to establish location coordinates. Two beacons could be soft-landed on the lunar surface at the limits of allowable separation and each would transmit a wide-beam signal with cones reaching GEO heights and be strong enough to be received by small antennae in near-earth orbit. The black box processor would perform on-board computation with one-way Doppler/range data and dynamical models. Alternatively, GEO satellites such as the GPS or TDRSS spacecraft can be used with interferometric techniques to provide decimeter-level accuracy for aircraft navigation.
Document ID
19830054834
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Khatib, A. R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Ellis, J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
French, J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Null, G.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Yunck, T.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Wu, S.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena CA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1983
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
AIAA PAPER 83-0351
Accession Number
83A36052
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other

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