NDLI: Estimation of dynamic characteristics of the International Space Station from measurements of microaccelerations

Content Provider	Springer Nature Link
Author	Zavalishin, D. A. Sazov, V. V. Belyev, M. Yu.
Copyright Year	2009
Abstract	We describe the results of determining the mass of the International Space Station using the data of MAMS accelerometer taken during correction of the station orbit on August 20, 2004. The correction was made by approach and attitude control engines (ACE) of the Progress transporting spacecraft. The engines were preliminary calibrated in an autonomous flight using the onboard device for measuring apparent velocity increment. The method of calibration is described and its results are presented. The error in station mass determination is about 1%. The same data of MAMS and similar data obtained during the orbit correction on August 26, 2004 were used for the analysis of high-frequency vibrations of the station mainframe caused by operation of the ACE of Progress. Natural frequencies of the ACE are determined. They lie in the frequency band 0.024–0.11 Hz. ACE operation is demonstrated to result in a substantial increase of microaccelerations onboard the station in the frequency range 0–1 Hz. The frequencies are indicated at which disturbances increase by more than an order of magnitude. The study described was carried out as a part of the Tensor technological experiment.
Ending Page	184
Page Count	12
Starting Page	173
File Format	PDF
ISSN	00109525
e-ISSN	16083075
Journal	Cosmic Research
Issue Number	2
Volume Number	47
Language	English
Publisher	SP MAIK Nauka/Interperiodica
Publisher Date	2009-04-23
Publisher Place	Dordrecht
Access Restriction	One Nation One Subscription (ONOS)
Subject Keyword	Extraterrestrial Physics, Space Sciences Astrophysics Astronomy, Astrophysics and Cosmology
Content Type	Text
Resource Type	Article
Subject	Astronomy and Astrophysics Aerospace Engineering Space and Planetary Science

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