ISSN 0021-3454 (print version)
ISSN 2500-0381 (online version)
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9
Issue
vol 63 / September, 2020
Article
UDC 519.2

ESTIMATION OF ACCURACY CHARACTERISTICS OF CARRIER ROCKET CONTROL SYSTEM BY RESULTS OF LAUNCHES UNDER VARIOUS CONDITIONS

V. N. Arseniev
A. F. Mozhaysky Military Spaсe Academy, Department of Onboard Information and Measuring Complexes; Professor


P. V. Labetsky
Mozhaysky Military Space Academy; Post-Graduate Student


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Abstract. The problem of estimation of accuracy characteristics of carrier rocket control system by results of field tests under various conditions is considered. A new approach to determination of the operator of the results reduction to uniform conditions is proposed. The approach is shown to improve the estimations accuracy.
Keywords: control system, carrier rocket, accuracy characteristics, rocket launch conditions, non-uniform data