DocumentCode
345018
Title
Modern concepts for avionics systems validation test environments
Author
Mayer, John T B ; Montanez, Leticia ; Roberts, James A. ; Graves, Ricky D.
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
Volume
1
fYear
1999
fDate
1999
Firstpage
441
Abstract
The Cassini Program is the last of the large interplanetary spacecraft missions. The Integration Test Laboratory (ITL) at the Jet Propulsion Laboratory (JPL) is part of the Cassini Program. This laboratory includes the Attitude and Articulation Control Subsystem (AACS) testbed. This environment was used to not only verify and validate the AACS but was also used to develop advanced concepts and ideas for use in future testbed environments. The concepts developed for the AACS testbed included the use of multiple computers, real-time data collection and real-time display. Internet access and the incorporation of commercially available components. These concepts resulted in improved simulation fidelity, repeatable operation and reduced future operational costs. This paper focuses on a description of the testbed, lessons learned, the innovations used and future directions that will substantially reduce future testbed costs
Keywords
Internet; aerospace computing; aerospace simulation; aerospace test facilities; attitude control; automatic test equipment; avionics; economics; real-time systems; space vehicle electronics; Attitude and Articulation Control Subsystem; COTS; Cassini Program; Integration Test Laboratory; Internet access; JPL; Jet Propulsion Laboratory; avionics; multiple computers; operational costs; real-time data collection; real-time display; repeatable operation; testbed costs; validation test; Aerospace electronics; Attitude control; Computational modeling; Computer displays; Costs; Internet; Laboratories; Propulsion; Space vehicles; System testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 1999. Proceedings. 1999 IEEE
Conference_Location
Snowmass at Aspen, CO
Print_ISBN
0-7803-5425-7
Type
conf
DOI
10.1109/AERO.1999.794351
Filename
794351
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