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Tracking and Orbit-Determination Program of the Jet Propulsion LaboratoryThe lunar-probe tracking program at the Jet Propulsion Laboratory has two prime objectives: (1) provide real-time predictions of the direction of the probe from various observation stations; (2) establish a reliable trajectory corresponding to the actual flight path of the probe. The tracking program, although developed for use with lunar probes, can be used for interplanetary probes if certain modifications are made. The program, as developed for the IBM 704 digital computer, has two distinct phases. First, the equations of motion and the variational equations are integrated to each observation time where the elements of the equation A (sub u) equals b [linearization of the maximum likelihood equations] are computed. The second phase is concerned with the solution of a specified subset of A (sub u) equals b. Flexibility and ease of operation have been major objectives in writing the 704 program. The number of data points and tracking stations that may be used is limited only by computing time and core storage. Input formats and operating instructions are presented for utilizing the various computational options available in the program.
Document ID
19630039027
Acquisition Source
Headquarters
Document Type
Other
Authors
Carr, Russell E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Hudson, R. Henry
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 1, 2013
Publication Date
February 22, 1960
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
JPL-TR-32-7
Report Number: JPL-TR-32-7
Accession Number
63N81910
Funding Number(s)
CONTRACT_GRANT: NASW-6
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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