For Libraries For Publication Open Access Downloads About Us Contact Us
Paper Titles
Stress Analysis of the Press Cage in Screw Press by Finite Element Method
p.164
Optimization Design of Engine Mounting System
p.168
Anisometry Anterior Cruciate Ligament Sport Injury Mechanism Study: A Finite Element Model with Optimization Method
p.173
Simulation of Artificial Lighting Comfort of Cab for High-Speed Train
p.181
Atmospheric Resistance Perturbation Analysis of Spacecraft Orbit
p.185
Modification of Spalart-Allmaras Turbulence Model for Predicting S825 Airfoil Aerodynamic Performance
p.189
Reliability Simulation and Forecast Based on Virtual Prototype for the Running System of Complicated Equipments
p.195
Stochastic Fatigue Reliability Analysis for Torsion Shaft of Military Tracked Vehicles
p.199
Research the Influence of Part State Sliding Surface on SMC Chattering
p.203

Atmospheric Resistance Perturbation Analysis of Spacecraft Orbit

Article Preview

Abstract:

The variation rules of middle and high level atmosphere affected by sun activity are analyzed, and atmosphere resistance perturbation acceleration models of spacecraft orbit are deduced. Atmosphere resistance perturbation is simulated by STK, and the parameters of spacecraft orbit affected by atmosphere resistance are got at different situation of sun activity. Finally, the life of spacecraft orbit is calculated.

You might also be interested in these eBooks
Vehicle, Mechatronics and Information Technologies II View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volumes 543-547)

Pages:

185-188

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.543-547.185

Citation:

Cite this paper

Online since:

March 2014

Authors:

Hai Yang Liu*, Lan Ying Zhang, Chuang Fang Li

Keywords:

Atmosphere Resistance, Life of Orbit, Perturbation, STK

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

© 2014 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

References

[1] Du Heng, Ye Zonghai. Space environment handbook of low LEO spacecraft, (1996).

Google Scholar

[2] Wang Peng. Research on modeling and simulation technologies of space environment elements based on HLA, (2006).

Google Scholar

[3] Gong Jiancun. Exposure of Solar Storm, 2011, pp.138-143.

Google Scholar

[4] Xi Xiaoning, Wang Wei. Fundamentals of near earth spacecraft orbit, (2003).

Google Scholar

[5] SPACE SECURITY 2007. Library and Archives Canada cataloguing in Publications Data.

Google Scholar

[6] Xu Fuxiang. Introduction of satellite engineering, (2003).

Google Scholar

© 2025 Trans Tech Publications Ltd. All rights are reserved, including those for text and data mining, AI training, and similar technologies. For open access content, terms of the Creative Commons licensing CC-BY are applied.
Scientific.Net is a registered trademark of Trans Tech Publications Ltd.