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INFLUENCE OF ORIENTATION MATRIX PARAMETERIZATION METHOD ON ORIENTATION PROBLEM SOLVING

S.A. Klimanova, A.V. Kramlikh

Samara National Research University, Samara

Formulating and solving spacecraft orientation problem it is convenient to introduce the right-handed orthogonal coordinate system (trihedron) with a center in a given point, as a rule, in an object’s center of mass. The following methods of orientation matrix parameterization became a frequent practice in solving an orientation problem:

-  parameterization applying Krylow, Euler angles, etc.;

-   parameterization using quaternions.

 References:

1. Branets, V.N. Applying quaternions in rigid body orientation problem [Text] / V.N. Branets, I.P. Shmyglevskiy.- Nauka, 1973. – pp. 320