On the attitude of a spacecraft near a Lagrangian point

Details On the attitude of a spacecraft near a Lagrangian point On the attitude of a spacecraft near a Lagrangian point

Sep 1989

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1989baicz..40..302a&link_type=abstract

Astronomical Institutes of Czechoslovakia, Bulletin (ISSN 0004-6248), vol. 40, no. 5, Sept. 1989, p. 302-307.

Astronomy and Astrophysics

Astronomy

1

Attitude (Inclination), Attitude Control, Lagrangian Equilibrium Points, Rotating Bodies, Three Body Problem, Canonical Forms, Equations Of Motion, Hamiltonian Functions, Quaternions

Scientific paper

The rotation of a rigid body which is moving near L(4) is considered.
Based upon Euler angles, an extended set of quaternions and its
conjugate moments is employed, and the canonical equations of the motion
are established. Finally, a numerical example is given.

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