Orbit Averaged Variation of Earth Satellite Orbital Elements

An orbit averaging numerical integration method for determining the variation in the shape and orientation of an earth satellite orbit is discussed.

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Bibliographic Details
Main Author: Ash, Michael E
Format: Report
Language:English
Subjects:
ELLIPTICAL ORBIT TRAJECTORIES
EQUATIONS OF MOTION
GEOMAGNETISM
GRAVITY
MATRICES(MATHEMATICS)
NUMERICAL INTEGRATION
PARTIAL DIFFERENTIAL EQUATIONS
Spacecraft Trajectories and Reentry
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Description
Summary:An orbit averaging numerical integration method for determining the variation in the shape and orientation of an earth satellite orbit is discussed.