Спутниковое навигационно-баллистическое обеспечение в задаче повышения точности инерциальной навигационной системы

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Спутниковое навигационно-баллистическое обеспечение в задаче повышения точности …
Инженерный журнал: наука и инновации # 9·2016 13
Satellite navigation and ballistic support in the problem
of improving inertial navigation system accuracy
© S.N. Ilyuhin, A.N. Klishin, O.S. Shvyrkina
Bauman Moscow State Technical University, Moscow, 105005, Russia
The article gives information on the fundamentals of inertial navigation system correc-
tion with data periodically received from the satellite navigation systems , substantiates
such corrections necessity, and illustrates the main types of inertial navigation system
errors. We consider the ways of using satellite navigation data to improve the spacecraft
flight accuracy. The study also describes in detail the inertial navigation system algo-
rithm and analyses its observability according to satellite navigation data. The object of
the study was to obtain an optimal recursive algorithm for estimating spacecraft coordi-
nates according to the satellite navigation system discrete data .
Keywords: inertial control system, satellite navigation system, observability, accuracy.
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Ilyukhin S.N. (b. 1990) graduated from Bauman Moscow State Technical University in
2013. Assistant, Department of Dynamics and Flight Control of Rockets and Spacecraft,
Bauman Moscow State Technical University. Author of 17 research publications in the
field of ballistics, space flight dynamics, space flight control, weapon history.
e-mail: