Zobrazeno 1 - 10
of 76
pro vyhledávání: '"attitude regulation"'
Publikováno v:
Electrical engineering & Electromechanics, Iss 5, Pp 17-23 (2021)
Introduction. Unmanned aerial vehicles as quadcopters, twin rotors, fixed-wing crafts, and helicopters are being used in many applications these days. Control approaches applied on the quadrotor after decoupling the model or separate altitude control
Externí odkaz:
https://doaj.org/article/cf25731c83aa48a18f55619f94b66abe
Publikováno v:
IEEE Access, Vol 9, Pp 159724-159733 (2021)
This article investigates a finite-time attitude control with chattering suppression for quadrotors based on a high-order extended state observer (HESO). To improve the anti-disturbance capacity of quadrotors, a HESO capable of estimating fast time-v
Externí odkaz:
https://doaj.org/article/d8d04df83a794e9da6065a364e40dee4
Publikováno v:
IEEE Access, Vol 7, Pp 93198-93211 (2019)
The attitude regulation of spacecraft using continuous time execution of the control law is not always affordable for the low-cost satellites with limited wireless resources. Of late, within the ambit of control of systems over networks, event-trigge
Externí odkaz:
https://doaj.org/article/05e53052ad1542e5882cd60c386c072d
Akademický článek
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Akademický článek
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Publikováno v:
IEEE Access, Vol 9, Pp 159724-159733 (2021)
This article investigates a finite-time attitude control with chattering suppression for quadrotors based on a high-order extended state observer (HESO). To improve the anti-disturbance capacity of quadrotors, a HESO capable of estimating fast time-v
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8773f4bbfb989691ebfa94a34319d64c
https://ieeexplore.ieee.org/document/9618938/
https://ieeexplore.ieee.org/document/9618938/
The attitude regulation problem with bounded control for a class of satellites in the presence of large disturbances, with bounded moving average, is solved using a Lyapunov-like design. The analysis and design approaches are introduced in the case i
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1ed1d23df47814f62af7a59632a85b89
http://hdl.handle.net/2108/303035
http://hdl.handle.net/2108/303035
The attitude regulation problem with bounded control for a class of satellites in the presence of large disturbances, with bounded moving average, is solved using a Lyapunov-like design. The analysis and design approaches are introduced in the case i
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______2659::53494880e6276164dde63d1ed68fb935
https://zenodo.org/record/6777962
https://zenodo.org/record/6777962
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2012, Vol. 84, Issue 5, pp. 321-329.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/00022661211255502
Publikováno v:
Electronics
Volume 10
Issue 14
Electronics, Vol 10, Iss 1709, p 1709 (2021)
Volume 10
Issue 14
Electronics, Vol 10, Iss 1709, p 1709 (2021)
This paper explores the problem of attitude stabilization of spacecraft under multiple uncertainties and constrained bandwidth resources. The proposed control law is designed by combining the sliding mode control (SMC) technique with a prescribed per
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::61867bd65187a65b314c8816a373703c