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1 Ergebnisse
1
Output Feedback Control for Spacecraft Attitude System with..:
Xuan-Mung, Nguyen
;
Golestani, Mehdi
;
Nguyen, Huu Tiep
..
Mathematics. 11 (2023) 9 - p. 2149 , 2023
Link:
https://doi.org/10.3390/math11092149
RT Journal T1
Output Feedback Control for Spacecraft Attitude System with Practical Predefined-Time Stability Based on Anti-Windup Compensator
UL https://suche.suub.uni-bremen.de/peid=cr-10.3390_math11092149&Exemplar=1&LAN=DE A1 Xuan-Mung, Nguyen A1 Golestani, Mehdi A1 Nguyen, Huu Tiep A1 Nguyen, Ngoc Anh A1 Fekih, Afef PB MDPI AG YR 2023 SN 2227-7390 JF Mathematics VO 11 IS 9 SP 2149 LK http://dx.doi.org/https://doi.org/10.3390/math11092149 DO https://doi.org/10.3390/math11092149 SF ELIB - SuUB Bremen
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