Analysis of Satellite Drag Coefficients Based on Physical and Orbital Specifications
Author:
Affiliation:
1. Space Strategies Consulting Ltd,Kanata,ON,Canada,K2L 3H1
2. Mechanical and Aerospace Engineering Clarkson University,Potsdam,NY,13699
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/9843190/9843194/09843417.pdf?arnumber=9843417
Reference26 articles.
1. Comparison and Accuracy Assessment of Semi-Empirical Atmosphere Models through the Orbital Decay of Spherical Satellites
2. A New Empirical Thermospheric Density Model JB2008 Using New Solar and Geomagnetic Indices
3. Static diffusion models of the upper atmosphere with empirical temperature profiles
4. NRLMSIS 2.0: A Whole‐Atmosphere Empirical Model of Temperature and Neutral Species Densities
5. Drag Coefficient Estimation in Orbit Determination
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