Title :
Dynamics and control of angular acceleration of a re-entry spacecraft with a small asymmetry in the atmosphere in the presence of the secondary resonance effect
Author_Institution :
Dept. of Higher Math., SSAU, Samara, Russia
Abstract :
We consider the problem of controlled reduction of angular acceleration of a re-entry spacecraft with a small mass and aerodynamic asymmetry. An analytical dependence is proposed to control the angular acceleration of the spacecraft, providing a reduction in the aerodynamic asymmetry.
Keywords :
acceleration control; aerodynamics; resonance; space vehicles; aerodynamic asymmetry; analytical dependence; angular acceleration control; atmosphere asymmetry; controlled reduction problem; mass asymmetry; re-entry spacecraft; secondary resonance effect; Acceleration; Aerodynamics; Angular velocity; Atmospheric modeling; Mathematical model; Space vehicles; angular velocity; asymmetry; control; resonance effect; spacecraft;
Conference_Titel :
Control and Communications (SIBCON), 2015 International Siberian Conference on
Conference_Location :
Omsk
Print_ISBN :
978-1-4799-7102-2
DOI :
10.1109/SIBCON.2015.7147134
