Performance Analysis of GPS Based Orbit Determination via Numerical Methods for a LEO Satellite

被引：0

作者：

Bagci, Murat ^{[1
]}

Hacizade, Cengiz ^{[2
]}

机构：

[1] Turkish Air Force Acad, Inst Space Technol & Aeronaut, TR-34149 Istanbul, Turkey

[2] Istanbul Tech Univ, Fac Aeronaut & Astronaut, TR-34469 Istanbul, Turkey

来源：

2015 7TH INTERNATIONAL CONFERENCE ON RECENT ADVANCES IN SPACE TECHNOLOGIES (RAST) | 2015年

关键词：

GPS; Newton-Raphson; Bancroft; Matlab fsolve;

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Determination and control of the satellite's orbit is acting vital role on space mission. Accuracy in calculations for position and velocity of such a satellite is important for fulfilling the tasks. The motion of a Low Earth Orbit (LEO) satellite can be modelled with Keplerian equations. In this study, we use Keplerian equations to construct dynamic model of LEO satellite and analyze performances of three numerical methods (Newton-Raphson, Bancroft and Matlab fsolve) in Global Positioning System (GPS) based trilateration problem solving

引用

页码：731 / 735

页数：5

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