Analytical Algorithm for Constructing the Orbital Orientation of a Spacecraft with an Incomplete Measurement of the State Vector Components
- Авторы: Zubov N.1, Lapin A.1, Ryabchenko V.1
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Учреждения:
- Bauman Moscow State Technical University
- Выпуск: Том 58, № 6 (2019)
- Страницы: 969-979
- Раздел: Control Systems of Moving Objects
- URL: https://journals.rcsi.science/1064-2307/article/view/220557
- DOI: https://doi.org/10.1134/S1064230719040178
- ID: 220557
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Аннотация
The problem of joint synthesis of a modal controller and observer is solved analytically for a sixth-order system that describes the rotational motion of a spacecraft with the available measurements of five components of the state vector. The modeling results that describe the application of the synthesized control and observation laws for the construction of the orbital orientation of a spacecraft are presented in the paper.
Об авторах
N. Zubov
Bauman Moscow State Technical University
Автор, ответственный за переписку.
Email: nik.zubov@gmail.com
Россия, Moscow, 105005
A. Lapin
Bauman Moscow State Technical University
Email: nik.zubov@gmail.com
Россия, Moscow, 105005
V. Ryabchenko
Bauman Moscow State Technical University
Email: nik.zubov@gmail.com
Россия, Moscow, 105005