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IssuesArchive of Issues2013-2pp.140-146

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V.I. Golovatenko-Abramov, "Optimal Technology of Inertial Measurements," Mech. Solids. 48 (2), 140-146 (2013)
Year 2013 Volume 48 Number 2 Pages 140-146
DOI 10.3103/S0025654413020040
Title Optimal Technology of Inertial Measurements
Author(s) V.I. Golovatenko-Abramov (4th Central Scientific Research Institute, Ministry of Defence of the Russian Federation, Tikhonravova 29, Yubileynyy, Moscow Oblast, 141080 Russia, vlagolab@mail.ru)
Abstract A technological project for measuring the spacecraft angular velocity vector is justified, the maximum accuracy is attained, and the proposed technology is compared with well-known methods for inertial measurements. The present paper is a continuation of [1].
Keywords uniaxial transducer, inertial gage unit, measurement vector, random vector distribution law, measurement technology, optimization
References
1.  V. I. Golovatenko-Abramov, "Optimal Excessive Geometric Structure of Spacecraft Inertial Measuring Tools," Kosmich. Issled. 31 (2), 100-107 (1993) [Cosmic Res. (Engl. Transl.)].
2.  B. V. Raushenbakh and E. N. Tokar', Spacecraft Attitude Control (Nauka, Moscow, 1974) [in Russian].
3.  V. I. Golovatenko-Abramov, Absolute Extremum. Search Algorithms (4th TsNII MO RF, 2004), p. 10 [in Russian].
Received 12 November 2010
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