N.V. Yefymenko
Èlektron. model. 2018, 40(6):21-35
https://doi.org/10.15407/emodel.40.06.021
ABSTRACT
A model of the rotational motion of a space vehicle in the form of a second-order differential equation with respect to the Rodrig-Hamilton paralleleters is considered. The properties of this equation are studied and a technique for the synthesis of spacecraft orientation algorithms is proposed, which makes it possible to find program trajectories of the reorientation of space vehicles. The results of experimental verification of the proposed technique on the Sich-2 spacecraft are presented.
KEYWORDS
Rodrig-Hamilton parameters, spacecraft, quaternion, orientation, dynamical equation for the quaternion.
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