检索 - Izvestiâ Akademii nauk. Rossijskaâ akademiâ nauk. Mehanika tverdogo tela.

Quaternion regularization of differential equations of perturbed central motion and regular models of orbital (trajectory) motion: review and analysis of models, their applications

Analytical solution of the problem of optimal control of reorientation of solid body (spacecraft), in sense of a combined criteria of quality, based on the quaternions

Quaternion regular equations of the two-body problem and the problem of the motion of a satellite in the gravitational field of the earth in the Kustaanheimo-Stifel variables and modified four-dimensional variables: dynamics of relative motion

Quaternion Methods and Regular Models of Celestial and Space Flight Mechanic: Using Euler (Rodrigues-Hamilton) Parameters to Describe Orbital (Trajectory) Motion. II: Perturbed Spatial Restricted Three-Body Problem

Quaternion Methods and Regular Models of Celestial Mechanics and Space Flight Mechanics: Local Regularization of the Singularities of the Equations of the Perturbed Spatial Restricted Three-Body Problem Generated by Gravitational Forces

Regular quaternion equations orbital motion in the earth’s gravitational field in KS-variables and their modifications. Reduction of dimensionality, first integrals of equations

Control of the Rotation of a Solid (Spacecraft) with a Combined Optimality Criterion Based on Quaternions