Zobrazeno 1 - 10
of 633
pro vyhledávání: '"Spacecraft attitude control"'
Autor:
Zhaoxiang Yi, Meng Jiang
Publikováno v:
Systems Science & Control Engineering, Vol 12, Iss 1 (2024)
This paper proposes a high-precision attitude cooperative control strategy for three spacecraft in space gravitational wave detection. Firstly, based on the layout of optical components on the spacecraft and factors such as external interference and
Externí odkaz:
https://doaj.org/article/3b06ebebf7b248ed85ddd42757e54c22
Publikováno v:
Symmetry, Vol 16, Iss 7, p 789 (2024)
This paper proposes a prescribed performance control policy for spacecraft attitude tracking control. The designed controller employs a kind of performance envelope function that can configure the convergence rate arbitrarily. Moreover, the controlle
Externí odkaz:
https://doaj.org/article/e6e2f1cdebdc4bc3a596aa498481e9b7
Publikováno v:
Measurement Science Review, Vol 23, Iss 4, Pp 146-153 (2023)
In this work, we build a satellite attitude Proportional-Integral-Derivative (PID) controlled system by using the Hubble Space Telescope (HST) parameters as a reference and tune its controller parameters using various tuning methods. First, we give t
Externí odkaz:
https://doaj.org/article/30883fdebc0e49a0a586f82da61eed26
Autor:
Dimitri Mahayana
Publikováno v:
IEEE Access, Vol 11, Pp 70238-70247 (2023)
The attitude dynamics of spacecraft are highly nonlinear, which makes it challenging to design control algorithms that can handle these nonlinearities. This study presents a novel data-driven synthesis method for spacecraft attitude control using the
Externí odkaz:
https://doaj.org/article/4b645bd29aa64efe94938a544314bfbf
Autor:
Weiqiang Tang
Publikováno v:
Systems Science & Control Engineering, Vol 10, Iss 1, Pp 126-133 (2022)
A novel attitude control algorithm is developed for spacecrafts based on the model predictive control and proportional-integral observer (PIO) in the presence of constraints. The high dimensional nonlinear dynamics are firstly transformed into three
Externí odkaz:
https://doaj.org/article/3832e75767804ea08ff1ddf00cdbf153
Publikováno v:
Aerospace, Vol 11, Iss 1, p 61 (2024)
Ball-shell rotors with non-standard shapes, non-uniform conductive coatings, and eccentric masses machined by conventional processes constrain the improvement of levitation and torque accuracy of magnetically levitated momentum balls. This paper focu
Externí odkaz:
https://doaj.org/article/a8c946b766ac444984de84cb0c5e6502
Akademický článek
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Akademický článek
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Publikováno v:
Aircraft Engineering and Aerospace Technology, 2021, Vol. 94, Issue 5, pp. 667-675.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-12-2020-0299
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2021, Vol. 94, Issue 2, pp. 248-254.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-06-2021-0184