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Radio metric direction finding - A new approach to deep space navigationThe paper explores an alternate technique for the determination of the angular position and velocity of deep-space probes, wherein the two-way range and Doppler measurements are abandoned for large portions of the mission in favor of differential one-way measurements. The spacecraft employs a wideband beacon rather than a coherent transponder, and differential measurements of one-way range and perhaps range rate are made between the spacecraft and each of three tracking stations. Advantages include the following: (1) Range measurements do not require the long horizon-to-horizon Doppler passes, so that the tracking stations can be released to support other functions of the deep space network. (2) Improved accuracy in the angular coordinates of the spacecraft can be obtained. (3) The need for an uplink is eliminated. A system implementation of the concept is developed that appears economically feasible and achieves a 0.05 microrad baseline accuracy
Document ID
19780047980
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Melbourne, W. G.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Curkendall, D. W.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Date Acquired
August 9, 2013
Publication Date
September 1, 1977
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Accession Number
78A31889
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other

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