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Advanced multilateration theory, software development, and data processing: The MICRODOT systemThe process of geometric parameter estimation to accuracies of one centimeter, i.e., multilateration, is defined and applications are listed. A brief functional explanation of the theory is presented. Next, various multilateration systems are described in order of increasing system complexity. Expected systems accuracy is discussed from a general point of view and a summary of the errors is listed. An outline of the design of a software processing system for multilateration, called MICRODOT, is presented next. The links of this software, which can be used for multilateration data simulations or operational data reduction, are examined on an individual basis. Functional flow diagrams are presented to aid in understanding the software capability. MICRODOT capability is described with respect to vehicle configurations, interstation coordinate reduction, geophysical parameter estimation, and orbit determination. Numerical results obtained from MICRODOT via data simulations are displayed both for hypothetical and real world vehicle/station configurations such as used in the GEOS-3 Project. These simulations show the inherent power of the multilateration procedure.
Document ID
19760026498
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Escobal, P. R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Gallagher, J. F.
(Computer Sciences Corp. Pasadena, CA, United States)
Vonroos, O. H.
(Jet Propulsion Lab., California Inst. of Tech.)
Date Acquired
September 3, 2013
Publication Date
July 4, 1976
Subject Category
Geosciences (General)
Report/Patent Number
NASA-CR-148839
JPL-TM-33-792
Report Number: NASA-CR-148839
Report Number: JPL-TM-33-792
Accession Number
76N33586
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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