Control of a spacecraft's spatial turn with minimum value of the path functional

Details Control of a spacecraft's spatial turn with minimum value of the path functional Control of a spacecraft's spatial turn with minimum value of the path functional

Jun 2007

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2007cosre..45..234l&link_type=abstract

Cosmic Research, Volume 45, Issue 3, pp.234-247

Mathematics

02.30.Yy

Scientific paper

The problem of optimal (with minimum value of the path functional) control over a spatial reorientation of a spacecraft is considered. Using the quaternion method, an analytical solution to this problem is obtained. For the symmetrical optimality index, the complete solution to the problem of spacecraft reorientation is represented in a closed form. The results of mathematical modeling of the spacecraft motion dynamics are presented, demonstrating the practical efficiency of the developed algorithm of control.

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