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NASA NTRS · 19640042572

Precession rates for an artificial satellite.

Anderson, J.·Lorell, J.

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Abstract

Long period component and secular component of satellite motion evaluated, using lagrange planetary equation

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GRAVITATIONAL FIELD LAGRANGE EQUATION SATELLITE ORBIT

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Anderson, J., Lorell, J.. 1964-01-01. Precession rates for an artificial satellite.. https://ntrs.nasa.gov/citations/19640042572

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