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Gravitational orientation of the orbital complex, Salyut-6--SoyuzA simple mathematical model is proposed for the Salyut-6-Soyuz orbital complex motion with respect to the center of mass under the one-axis gravity-gradient orientation regime. This model was used for processing the measurements of the orbital complex motion parameters when the above orientation region was implemented. Some actual satellite motions are simulated and the satellite's aerodynamic parameters are determined. Estimates are obtained for the accuracy of measurements as well as that of the mathematical model.
Document ID
19840008160
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Grecho, G. M. (NASA Headquarters Washington, DC United States)
Sarychev, V. A. (NASA Headquarters Washington, DC United States)
Legostayev, V. P. (NASA Headquarters Washington, DC United States)
Sazonov, V. V. (NASA Headquarters Washington, DC United States)
Gansvind, I. N. (NASA Headquarters Washington, DC United States)
Date Acquired
September 4, 2013
Publication Date
October 1, 1983
Subject Category
Astrodynamics
Report/Patent Number
NAS 1.15:77299
NASA-TM-77299
Report Number: NAS 1.15:77299
Report Number: NASA-TM-77299
Accession Number
84N16228
Funding Number(s)
CONTRACT_GRANT: NASW-3541
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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