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This article is cited in 1 scientific paper (total in 1 paper)
Coordinate and time-frequency support of a spacecraft flight by means of autonomic navigation using sigma-point Kalman filter algorithm
Vladimir A. Filimonov, Vyacheslav V. Shavrin, Vladimir I. Tislenko, Alexey P. Kravets, Vitaliy Yu. Lebedev, Vadim N. Shkolniy Research Institute of Radiotechnic Systems,
Tomsk State University of Control Sytems and Radioelectronics,
Lenina, 40, Tomsk, 634050, Russia
Abstract:
There are investigated errors of a spacecraft current coordinate and velocity estimates, time-frequency scale bias of the board receiver reference oscillator. The receiver is a component of the autonomic navigation system using signals of global navigation systems GLONASS or GPS. Estimates are formed by the navigation calculator on the bases of pseudo range and pseudo velocity measurements taken in the regime of navigation signals delay and Doppler frequencies tracking under the condition of the receiver noise. The calculator utilizes sigma-point Kalman filter. Analysis of estimations accuracy is done by the Monte-Carlo method while spacecraft moves along a high elliptic orbit.
Keywords:
autonomic navigation system, spacecraft, coordinate estimation, on board time scale bias, sigma-point Kalman filter, statistic simulation.
Received: 20.09.2015 Received in revised form: 26.10.2015 Accepted: 11.11.2015
Citation:
Vladimir A. Filimonov, Vyacheslav V. Shavrin, Vladimir I. Tislenko, Alexey P. Kravets, Vitaliy Yu. Lebedev, Vadim N. Shkolniy, “Coordinate and time-frequency support of a spacecraft flight by means of autonomic navigation using sigma-point Kalman filter algorithm”, J. Sib. Fed. Univ. Math. Phys., 8:4 (2015), 385–393
Linking options:
https://www.mathnet.ru/eng/jsfu442 https://www.mathnet.ru/eng/jsfu/v8/i4/p385
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Abstract page: | 196 | Full-text PDF : | 77 | References: | 40 |
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