Основы динамики космических аппаратов = Fundamentals of spacecraft dynamics

Описание

he study guide considers vibration disturbances, sources and levels acting on structural elements of the spacecraft, and the requirements for the vibration environment on the spacecraft. A brief overview of the forces and moments acting on the spacecraft in flight is given. The equations of disturbed motion of an absolutely rigid spacecraft in active flight segments and the laws of spacecraft control, as well as criteria, formulations and stability conditions are described. The pitch and yaw transfer functions acting on the spacecraft are presented. Experimental studies of structural elements of a fuel tank partially filled with a liquid have been carried out. The study guide is intended for senior students training in the direction of specialty 24.03.01 “Rocket systems and cosmonautics”, studying the discipline “Spacecraft Dynamics”.