DocumentCode :
2553371
Title :
Satellite ultraquiet isolation technology experiment (SUITE)
Author :
Anderson, Eric H. ; Fumo, John P. ; Erwin, R. Scott
Author_Institution :
CSA Eng. Inc., Mountain View. CA, USA
Volume :
4
fYear :
2000
fDate :
2000
Firstpage :
299
Abstract :
An experimental active vibration isolation called Satellite Ultraquiet Isolation Technology Experiment (SUITE) is described in detail. SUITE is a piezoelectric-based technology demonstration scheduled to fly in 2000 or 2001 on board the PICOSat spacecraft. SUITE is designed to show that the effect of small vibrations on spacecraft instrument effectiveness can be reduced significantly. Control from the ground station is planned for the first year after launch. A description of the PICOSat spacecraft and the other considerations influencing the development of the flight hardware begins the paper. Experiment goals are listed. The mechanical and electromechanical construction of the SUITE hexapod assembly is described, including the piezoelectric actuators, motion sensors, and electromagnetic actuators. The data control system is also described, including the digital signal processor and spacecraft communication. The main features of the software used for real-time control and the supporting Matlab software used for control system development and data processing are summarized. Initial test results are presented
Keywords :
aerospace computing; aerospace control; aerospace instrumentation; piezoelectric actuators; vibration isolation; Matlab software; PICOSat spacecraft; Satellite Ultraquiet Isolation Technology Experiment; active vibration isolation; data control; data processing; electromagnetic actuators; electromechanical construction; mechanical construction; motion sensors; piezoelectric actuators; piezoelectric technology; real-time control; satellite ultraquiet isolation technology; sensor conditioning; spacecraft instrument effectiveness; Communication system control; Control systems; Hardware; Instruments; Isolation technology; Piezoelectric actuators; Satellite ground stations; Space technology; Space vehicles; Vibrations;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference Proceedings, 2000 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
0-7803-5846-5
Type :
conf
DOI :
10.1109/AERO.2000.878441
Filename :
878441
Link To Document :
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