Different derivations of the kinematic equation for the rotation vector are discussed within a common framework. Simpler and more direct derivations of this kinematic equation are presented than are found in the literature. The kinematic equation is presented in terms of both the body-referenced angular velocity and the inertially referenced angular velocity. The kinematic equation is shown to have the same form in both the passive and active descriptions of attitude.<>
The kinematic equation for the rotation vector
IEEE Transactions on Aerospace and Electronic Systems ; 29 , 1 ; 263-267
01.01.1993
739499 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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