Mathematical Model of an the Angular Motion of a Solid Body in the Parameters of the Rodrig-Hamilton and its use in the Tasks of Control Spacecraft Orientation by N. V. Efimenko

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Mathematical Model of the Angular Motion of a Spacecraft in the Rodrig-Hamilton Parameters and Its Properties by N. V. Efimenko

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Synthesis of time-optimal three-dimensional rotation of spacecraft using rotational motion of equation of rigid body at Rodrigues–Hamilton parameters by N. V. Efimenko

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Synthesis of control algorithms of the spacecraft spatial reori-entation with the use of dynamic equations of a solid body rotational mo-tion in Rodrigo–Hamilton parameters by N. V. Efimenko

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Spacecraft angular motion control based on vector measurements by N. V. Efimenko, N. V. Lutsenko

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Determination of the parameters of the angular motion of the spacecraft from the information of the star sensor using the dynamic equation of the solid body rotation in the Rodrig–... by N. V. Efimenko, N. V. Lutsenko

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