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Information Journal Paper

Title

ORBIT DETERMINATION VIA A DEEPLY- COUPLED UKF/GNSS FILTER

Pages

  13-26

Keywords

UNSCENTED KALMAN FILTER (UKF)Q1

Abstract

 This paper is dedicated to determining the orbit of a satellite by using Unscented Kalman Filter (UKF), in which, a GNSS is used as the observation sensor. During this goal, firstly we have simulated the satellite orbit; considering oblations effect. Secondly, exploiting a nonlinear model of orbit dynamics, preliminary orbit determination is prepared via UKF algorithm. The range between the satellites and space vehicle as the parameter of observation in the filter is obtained. Afterwards, the estimated preliminary output data is corrected and more precise position of the GNSS satellite is determined based on predicted observations errors. Consequently, the outcomes of the research exhibits the acceptable satellite orbit determination error range.

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    APA: Copy

    AMIRI ATASHGAH, MOHAMMADALI, GAZERPOUR, HAMID, & ROGHANGIR, S.A.REZA. (2016). ORBIT DETERMINATION VIA A DEEPLY- COUPLED UKF/GNSS FILTER. JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST), 9(3 ), 13-26. SID. https://sid.ir/paper/149884/en

    Vancouver: Copy

    AMIRI ATASHGAH MOHAMMADALI, GAZERPOUR HAMID, ROGHANGIR S.A.REZA. ORBIT DETERMINATION VIA A DEEPLY- COUPLED UKF/GNSS FILTER. JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST)[Internet]. 2016;9(3 ):13-26. Available from: https://sid.ir/paper/149884/en

    IEEE: Copy

    MOHAMMADALI AMIRI ATASHGAH, HAMID GAZERPOUR, and S.A.REZA ROGHANGIR, “ORBIT DETERMINATION VIA A DEEPLY- COUPLED UKF/GNSS FILTER,” JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST), vol. 9, no. 3 , pp. 13–26, 2016, [Online]. Available: https://sid.ir/paper/149884/en

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