SATELLITE TRACKING PARAMETERS CALCULATION USING SGP4 MODELS

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DANESHNIA EHSAN; NASIRIAN MEHRZAD

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Journal: ELECTRONIC INDUSTRIES Year:2011 | Volume:2 | Issue:3 (7) Page(s): 37-52

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Information Journal Paper

Title

SATELLITE TRACKING PARAMETERS CALCULATION USING SGP4 MODELS

Author(s)

DANESHNIA EHSAN | NASIRIAN MEHRZAD | Issue Writer Certificate

Keywords

SATELLITE TRACKINGQ3

TRACKING PARAMETERSQ3

SGP4 MODEL VALIDATION TIMEQ3

Abstract

One of the most important subjects in the productivity of the satelliteis its guiding, controlling and tracking by ground stations. The satellite trajectory simulator is one of the tracking requirements in the ground station control unit. The satellite trajectories due time are undergone by various disturbances. This paper presents necessary formula using SGP algorithm and models the necessary calculation to simulating the disturbance effect on the orbit. The purpose of this paper is, error analyzing of this model with J2 model and two-body modelduring the third week. Error analysis and experimental test results using this algorithm show that the tracking accuracy of antenna with the 40 beam during this time is acceptable.

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APA: Copy

DANESHNIA, EHSAN, & NASIRIAN, MEHRZAD. (2011). SATELLITE TRACKING PARAMETERS CALCULATION USING SGP4 MODELS. ELECTRONIC INDUSTRIES, 2(3 (7)), 37-52. SID. https://sid.ir/paper/229700/en

Vancouver: Copy

DANESHNIA EHSAN, NASIRIAN MEHRZAD. SATELLITE TRACKING PARAMETERS CALCULATION USING SGP4 MODELS. ELECTRONIC INDUSTRIES[Internet]. 2011;2(3 (7)):37-52. Available from: https://sid.ir/paper/229700/en

IEEE: Copy

EHSAN DANESHNIA, and MEHRZAD NASIRIAN, “SATELLITE TRACKING PARAMETERS CALCULATION USING SGP4 MODELS,” ELECTRONIC INDUSTRIES, vol. 2, no. 3 (7), pp. 37–52, 2011, [Online]. Available: https://sid.ir/paper/229700/en

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