Drag Coefficient Model to Track Variations due to Attitude and Orbital Motion

What is it about?

Modeling the interaction between the satellite surface and atmosphere is important when determining the location of the satellite in orbit. This interaction can be characterized by a parameter called the drag coefficient which depends on various factors such as the satellite orientation and ambient parameters. We develop a model for the drag coefficient that can track the variations due to these factors and help us better determine the location of a satellite in orbit.

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