DocumentCode :
2567192
Title :
Attitude determination and control suitable for micro-spacecraft
Author :
Smith, Jay L.
Author_Institution :
Center for Aerosp. Technol., Weber State Univ., Ogden, UT, USA
Volume :
7
fYear :
2000
fDate :
2000
Firstpage :
143
Abstract :
The Center for AeroSpace Technology (CAST) at Weber State University, and One Stop Satellite Solutions Inc. (OSSS), in partnership with the United States Air Force Academy, has been developing the JAWSAT (Joint Air Force Academy Weber Satellite) for several years. It is currently manifest for launch January 2000 on the maiden flight of a converted minuteman rocket. CAST proposes using excess capabilities of the JAWSAT mission to demonstrate low-cost three-axis attitude determination and control. JAWSAT´s two-year mission will be to demonstrate the feasibility of launching multiple satellites from one low-cost carrier and to test low-cost microsat missions with advanced capabilities. JAWSAT will employ an ensemble of newly developed space hardware designed specifically for micro-satellite applications. This hardware includes three-axis attitude determination and control with diverse sensors and actuators, multi-band and multi-form communications, advanced structural design and fabrication, extensive software, and advanced video imaging
Keywords :
artificial satellites; attitude control; CAST; Center for AeroSpace Technology; JAWSAT; Joint Air Force Academy Weber Satellite; OSSS; One Stop Satellite Solutions; United States Air Force Academy; Weber State University; attitude control; low-cost carrier; low-cost three-axis attitude determination; micro-spacecraft; multi-form communication; multiple satellites; structural design; video imaging; Actuators; Application software; Communication system control; Fabrication; Hardware; Image sensors; Position measurement; Rockets; Satellites; Testing;
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.2000.879284
Filename :
879284
Link To Document :
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