Orientation and Resonance Locks for Satellites in the Elliptic Orbit

Details Orientation and Resonance Locks for Satellites in the Elliptic Orbit Orientation and Resonance Locks for Satellites in the Elliptic Orbit

Dec 1972

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1972cemec...6..421l&link_type=abstract

Celestial Mechanics, Volume 6, Issue 4, pp.421-424

Physics

Scientific paper

In order to achieve the maximum strength of higher resonance locks for satellites in the elliptic orbit, the condition of satellite orientation during the process of deployment is established. It is shown that for maximum strength locks the axis of the minimum moment of inertia of satellites should point toward the attracting body at ±(5/8) π and 0 values of the true anomalyf. This condition of deployment is applicable to all cases of resonance rotation regardless of the value of lock numberk and orbit eccentricitye.

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