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Attitude stabilization of a rigid spacecraft in the geomagnetic field
(Elsevier B.V., 2007-01-01)
An analytical method is proposed to study the attitude stability of a triaxial spacecraft moving in a circular Keplerian orbit in the geomagnetic field. The method is developed based on the electrodynamics effect of the ...
Attitude stabilization of a rigid spacecraft in the geomagnetic field
(Elsevier B.V., 2007-01-01)
An analytical method is proposed to study the attitude stability of a triaxial spacecraft moving in a circular Keplerian orbit in the geomagnetic field. The method is developed based on the electrodynamics effect of the ...
Attitude stabilization of a rigid spacecraft in the geomagnetic field
(Elsevier B.V., 2014)
Tethered slingshot maneuver in the three-dimensional space
(2018-01-01)
The Tethered Slingshot maneuver (TSSM) is an alternative solution to maneuver a spacecraft in space, which is based in the use of cables. A space tether usually consists in two fixed objects at the end of a cable. In this ...
Modeling, simulation, and control of the spacecraft attitude dynamics
(Universidad EAFIT, 2021-03-26)
Based on the three-dimensional dynamics of a rigid body and Newton’s laws, the simplified dynamics of a spacecraft is
studied and described through the systematical representation, mathematical modeling and also by a block ...
Effect of tides on the orbital evolution of the redback system PSR 1723–2837
(Wiley Blackwell Publishing, Inc, 2021-12)
The standard model of stellar evolution in Close Binary Systems assumes that duringmass transfer episodes the system is in a synchronised and circularised state. Remarkably, theredback system PSR J1723-2837 has an orbital ...
Zero, minimum and maximum relative radial acceleration for planar formation flight dynamics near triangular libration points in the Earth-Moon system
(Elsevier B.V., 2014-11-01)
Assume a constellation of satellites is flying near a given nominal trajectory around L-4 or L-5 in the Earth-Moon system in such a way that there is some freedom in the selection of the geometry of the constellation. We ...
Analytic and Geometric Techniques for Non-Integrable Dynamical Systems. Applications to Perturbed Keplerian Models.
(2020)
The present work using analytic and geometric methods to study differential
equations and systems of differential equations. Although some of the tools
developed here are intended to be applied to arbitrary equation, the ...