The use of the linear form of dynamical equations of the satellite attitude control system for its analysis and synthesis
1 |
AALR “Institute of Space Technique and Technology”, Almaty, Kazakhstan |
2 |
Al-Farabi Kazakh National University, Almaty, Kazakhstan |
CORRESPONDING AUTHOR
Anna Sukhenko
Laboratory of space systems development, Institute of space technique and technology, Kazakhstan
Submission date: 2020-06-04
Final revision date: 2020-08-26
Acceptance date: 2020-09-25
Online publication date: 2020-11-28
Publication date: 2021-01-15