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    Long-term motion of resonant satellites with arbitrary eccentricity and inclination (1982)
    In:  Other Sources
    Details
    Publication Date: 2011-08-18
    Description: A first-order, semi-analytical method for the long-term motion of resonant satellites is introduced. The method provides long-term solutions, valid for nearly all eccentricities and inclinations, and for all commensurability ratios. The method allows the inclusion of all zonal and tesseral harmonics of a nonspherical planet. We present here an application of the method to a synchronous satellite including J2 and J22 harmonics. Global, long-term solutions for this problem are given for arbitrary values of eccentricity, argument of perigee and inclination.
    Keywords: ASTRODYNAMICS
    Type: Celestial Mechanics; 27; Aug. 198
    Format: text
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