Quaternion Models and Algorithms for Solving the General Problem of Optimal Reorientation of Spacecraft Orbit

Autor: Ilya Alekseevich Pankratov, Yuriy Nikolaevich Chelnokov, Yakov Grigoryevich Sapunkov

Publikováno v: Известия Саратовского университета. Новая серия. Серия Математика. Механика. Информатика, Vol 20, Iss 1, Pp 93-104 (2020)

The problem of optimal reorientation of the spacecraft orbit is considered in quaternion formulation. Control (vector of the acceleration of the jet thrust) is limited in magnitude. To solve the problem it is required to determine the optimal orienta

Externí odkaz: https://doaj.org/article/fe60f56e5bad46fd8bd3c6bc54012406