Bezsilla, János and Takarics, Béla and Vanek, Bálint and Guo, Jian (2022) Parameter Uncertainty Analysis in Precise Pointing Control of Flexible Spacecraft. IFAC-PAPERSONLINE. ISSN 2405-8963 (In Press)
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BezsillaEtAl_MATHMOD22_ParameterUncertaintyAnalysisInPrecisePointingControlOfFlexibleSpacecraft.pdf Available under License Creative Commons Attribution Non-commercial No Derivatives. Download (616kB) | Preview |
Abstract
This article focuses on the validation of a classical PID controller scheme for flexible spacecraft with regards to the effect of parameter uncertainty on system stability and pointing precision. A high-fidelity simulation environment with external disturbances was built in Simulink using a control-oriented model of an Earth-observing satellite with a flexible appendage and on-board microvibration sources in orbit around the planet. Then, a PID control loop was designed with sensor dynamics, time delay behaviour, and a smooth trajectory generator. After declaring the natural frequencies, damping ratio, and rotation angle of the appendage, as well as the propellant tank mass to be uncertain, two worst-case scenarios were identified. Comparing the response of worst-case systems with nominal settings, only a minor drop has been found in the phase margins, with little to no difference in the pointing errors (smaller than ±2 arcsec for both roll and pitch).
Item Type: | Article |
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Subjects: | T Technology / alkalmazott, műszaki tudományok > TJ Mechanical engineering and machinery / gépészmérnöki tudományok |
Depositing User: | Béla Takarics |
Date Deposited: | 29 Sep 2022 08:08 |
Last Modified: | 03 Apr 2023 08:04 |
URI: | http://real.mtak.hu/id/eprint/150458 |
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