Vibration suppression of flexible spacecraft during attitude maneuvers

Journal of Guidance, Control, and Dynamics

Volumn 28, Issue 2, 2005, Pages 377-380

  Hu, Qinglei ^a,b   Ma, Guangfu ^a,b  

^a HARBIN INSTITUTE OF TECHNOLOGY   (China)

^b Dept of Contr Sci and Engineering ^*  (China)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; COMPUTER SIMULATION; DAMPING; LEAD COMPOUNDS; MANEUVERABILITY; MATHEMATICAL MODELS; MATRIX ALGEBRA; METHOD OF MOMENTS; OPTIMIZATION; PIEZOELECTRIC MATERIALS; PULSE WIDTH MODULATION; ROBUSTNESS (CONTROL SYSTEMS); SENSORS; TWO TERM CONTROL SYSTEMS; VECTORS; VIBRATION CONTROL;

COMPONENT SYNTHESIS VIBRATION SUPRESSION (CSVS) METHOD; LEAD ZIRCONATE TITANATE (PZT); PULSE-WIDTH PULSE-FREQUENCY (PWPF) MODULATION; VIBRATION SUPPRESSION;

SPACECRAFT;

EID: 15744380994     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.12967     Document Type: Article

References (9)

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