Optimal control of spacecraft motion in the Newtonian gravitational field: application of quaternions to describe orbit orientation.

Details Optimal control of spacecraft motion in the Newtonian gravitational field: application of quaternions to describe orbit orientation. Optimal control of spacecraft motion in the Newtonian gravitational field: application of quaternions to describe orbit orientation.

Aug 1999

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1999kosis..37..433c&link_type=abstract

Kosmicheskie Issledovaniia, Tom 37, No. 4, p. 433 - 442

Physics

Artificial Satellites: Orbit Theory, Artificial Satellites: Orientation

Scientific paper

The problem of rendezvous of a controllable spacecraft with a spacecraft
moving along a Keplerian orbit is solved. Four variants of solutions to
the problem and specific cases of the problem solution are considered.

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