Solar sailcraft motion in sun-earth-moon space with application to lunar transfer from geosynchronous orbit

Details Solar sailcraft motion in sun-earth-moon space with application to lunar transfer from geosynchronous orbit Solar sailcraft motion in sun-earth-moon space with application to lunar transfer from geosynchronous orbit

Aug 1992

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992wadc.iafcw....s&link_type=abstract

IAF, International Astronautical Congress, 43rd, Washington, Aug. 28-Sept. 5, 1992. 19 p.

Astronomy and Astrophysics

Astronomy

Attitude Control, Earth-Moon System, Equations Of Motion, Flyby Missions, Solar Sails, Solar System, Computer Programs, Geosynchronous Orbits, Interplanetary Trajectories, Mathematical Models, Spacecraft Configurations, Spherical Coordinates, Three Dimensional Models, Transfer Orbits

Scientific paper

A three-dimensional model of the dynamics of a solar sailcraft in the earth-sun-moon system is developed. The model includes derivations of a unit vector describing the direction of the resultant radiation force for a spectrally reflecting sail, the equations of motion for the sailcraft and the moon in spherical coordinates, and generalized equations for the initial conditions of the sailcraft in terms of orbit parameters, as well as the development of attitude control equations for the sail. A computer program based on this model, which includes a search routine, is used to investigate the problem of transfer to the moon from a geosynchronous orbit. Results are presented for two types of lunar encounters and the values of the sailcraft's area-to-mass ratio.

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