Vibration suppression of flexible spacecraft during attitude control

Acta Astronautica

Volumn 49, Issue 2, 2001, Pages 73-83

  Song, Gangbing ^a   Agrawal, Brij N ^b  

^a University of Akron   (United States)

^b NAVAL POSTGRADUATE SCHOOL   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; FEEDBACK CONTROL; MICROACTUATORS; MICROSENSORS; PIEZOELECTRIC DEVICES; POSITION CONTROL; PULSE WIDTH MODULATION; VIBRATIONS (MECHANICAL);

ATTITUDE CONTROL;

SPACECRAFT;

EID: 0035395228     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0094-5765(00)00163-6     Document Type: Article

References (13)

1. Attitude stability of flexible spacecraft which use dual time constant feedback lag network pseudorate control
2. Limit cycle oscillations in pulse modulated systems
3. Multiaxis tracking and attitude control of flexible spacecraft with reaction jets
4. Attitude stabilization of flexible spacecraft during station keeping maneuvers
5. Pulse-modulated control synthesis for a flexible spacecraft
6. Spacecraft vibration reduction using pulse-width pulse-frequency modulated input shaper
7. On the stability problem caused by finite actuator dynamics in the collocated control of large space structure
8. Positive position feedback control for large space structure
9. Adaptive structure for large precision antennas
10. Vibration suppression of a spacecraft flexible appendage using smart material
11. Experimental study of vibration suppression of flexible structure using modular control patch