Hs. Morton, HAMILTONIAN AND LAGRANGIAN FORMULATIONS OF RIGID-BODY ROTATIONAL-DYNAMICS BASED ON THE EULER PARAMETERS, The Journal of the astronautical sciences, 41(4), 1993, pp. 569-591
The orientation of an arbitrary rigid body is specified in terms of th
e set of four Euler parameters. A corresponding set of four generalize
d angular momentum variables is derived and then used to replace the u
sual three-component angular velocity vector in specifying the rate of
change of orientation of the body with respect to an inertial frame.
Through the use of Euler's equations, this leads naturally to a formul
ation of rigid body rotational dynamics in terms of a system of eight
first-order coupled differential equations involving the four Euler pa
rameters and the four conjugate momenta. These equations, expressed in
matrix form, are recognizable as Hamilton's canonical equations, and
exhibit a remarkable symmetry. A set of four second-order coupled diff
erential equations for the Euler parameters is also derived, and the e
quations are recognizable as Lagrange's equations. The sets of differe
ntial equations are solved numerically for a representative case of to
rque-free motion and the results are presented graphically.