Development of an Orbit Analysis Tool for LEO Satellites

被引：0

作者：

Kameche, Mohamed ^{[1
]}

Meghabber, Mohammed A. ^{[1
]}

Benzeniar, Haider ^{[1
]}

Boudjemai, Abdelmadjid ^{[1
]}

Himeur, Abdelaziz ^{[1
]}

Chikouche, Abdelwahab ^{[1
]}

机构：

[1] Ctr Dev Satellites ASAL, Ibn Rocd USTO, Oran 31130, Algeria

来源：

PROCEEDINGS OF 6TH INTERNATIONAL CONFERENCE ON RECENT ADVANCES IN SPACE TECHNOLOGIES (RAST 2013) | 2013年

关键词：

atmospheric density; JACCHIA; 70; NRL-MSIS00; mission analysis; maneuver; station keeping;

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

After the successful experiences of the two first earth observation satellites ALSAT-1 and ALSAT-2A, launched respectively, in November 2002 and July 2010, the Satellites Development Centre started developing mission analysis tools to be used for the future mission planed by the Algerian Space Agency. In this paper, we focus on the preliminary orbit analysis which represents a critical parameter for the feasibility and the definition of a space mission. The results of orbit analysis are used in the design of the payload, the propulsion and the communication subsystems and to guarantee that the defined ground track and local solar time control windows allow in addition to the quality of the mission data, the station keeping of the satellite in its reference orbit over the lifetime period and the required fuel for de-orbiting the satellite at the end of life.

引用

页码：241 / 246

页数：6

共 6 条

[1]

Benzeniar H., 2013, 9 IAA S SMA IN PRESS

[2]

Himeur A., 2013, 9 IAA S SMA IN PRESS

[3]

Kameche M., 2011, J AEROSPACE ENG, V3, P67

[4]

Kameche M., 2012, 23 INT S SPAC FLIGHT

[5] Analysis of the orbital decay of spherical satellites using different solar flux proxies and atmospheric density models [J].

Pardini, C ;

Tobiska, WK ;

Anselmo, L .

THERMOSPHERIC-IONOSPHERIC-GEOSPHERIC (TIGER) SYMPOSIUM, 2006, 37 (02) :392-400

[6]

Parsad R., 2001, ACTA ASTAUNOTICA, V48, P579

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