Development of Control Algorithms for the Orbital Motion of a Small Technological Spacecraft with a Shadow Portion of the Orbit

Abstract

The paper proposes algorithms for controlling the orbital motion of a small spacecraft for executive bodies with constant and variable thrust. The developed algorithms are aimed at neutralizing the influence of temperature shock on the level of microaccelerations in the area of technological equipment. The influence of the most significant part of the disturbances associated with a change in the size of large elastic elements as a result of temperature shock is leveled out. The developed algorithms can be used in the implementation of technological spacecraft projects such as the “Foton”, “Bion”, SJ series as well as promising small spacecraft such as Vozvrat-MKA.