The use of Euler parameters in the rotation of a satellite near L4

Details The use of Euler parameters in the rotation of a satellite near L4 The use of Euler parameters in the rotation of a satellite near L4

Dec 1986

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1986esasp.255..335a&link_type=abstract

In ESA Proceedings of the Second International Symposium on Spacecraft Flight Dynamics p 335-338 (SEE N87-25354 19-18)

Computer Science

Euler Equations Of Motion, Libration, Satellite Rotation, Spacecraft Motion, Three Body Problem, Hamiltonian Functions, Parameterization

Scientific paper

The rotational motion of a rigid body satellite whose center of mass is
moving near the libration point L4 is studied using the Euler
parameters. The Hamiltonian form of the equations of motion is obtained,
and inherent difficulties of the problem (singularities, triaxial
complexity, etc) do not appear.

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