Analytical Algorithm for Constructing the Orbital Orientation of a Spacecraft with an Incomplete Measurement of the State Vector Components
- Autores: Zubov N.E.1, Lapin A.V.1, Ryabchenko V.N.1
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Afiliações:
- Bauman Moscow State Technical University
- Edição: Volume 58, Nº 6 (2019)
- Páginas: 969-979
- Seção: Control Systems of Moving Objects
- URL: https://journal-vniispk.ru/1064-2307/article/view/220557
- DOI: https://doi.org/10.1134/S1064230719040178
- ID: 220557
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Resumo
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.
Sobre autores
N. Zubov
Bauman Moscow State Technical University
Autor responsável pela correspondência
Email: nik.zubov@gmail.com
Rússia, Moscow, 105005
A. Lapin
Bauman Moscow State Technical University
Email: nik.zubov@gmail.com
Rússia, Moscow, 105005
V. Ryabchenko
Bauman Moscow State Technical University
Email: nik.zubov@gmail.com
Rússia, Moscow, 105005
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