DocumentCode :
3401174
Title :
State modeling and pass automation in spacecraft control
Author :
Klein, Jim ; Kulp, Dan ; Rashkin, Bob
Author_Institution :
Computer Sci. Corp., Lanham-Seabrook, MD, USA
fYear :
1996
fDate :
22-24 Oct 1996
Firstpage :
52
Lastpage :
58
Abstract :
The Integrated Monitoring and Control COTS System (IMACCS) was developed as a proof-of-concept to show that commercial off-the-shelf (COTS) products could be integrated to provide spacecraft ground support faster and cheaper than current practices. A key component of IMACCS is the Altair Mission Control System (AMCS), one of several commercial packages available for satellite command and control. It is distinguished from otherwise similar tools by its implementation of Finite State Modeling as part of its expert system capability. Using the Finite State Modeling and State Transition capabilities of the ALTAIR Mission Control System (AMCS), IMACCS was enhanced to provide automated monitoring, routine pass support, anomaly resolution, and emergency “lights on again” response. Orbit determination and production of typical flight dynamics products, such as acquisition times and vectors, have also been automated
Keywords :
aerospace control; computerised monitoring; ground support systems; satellite telemetry; state estimation; Altair Mission Control System; COTS; Finite State Modeling; IMACCS; Integrated Monitoring and Control; State Transition; acquisition times; anomaly resolution; automated monitoring; commercial off-the-shelf products; commercial packages; emergency; flight dynamics products; orbit determination; routine pass support; satellite command and control; spacecraft ground support; vectors; Automatic control; Automation; Command and control systems; Control systems; Expert systems; Ground support; Monitoring; Packaging; Satellites; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
WESCON/96
Conference_Location :
Anaheim, CA
ISSN :
1095-791X
Print_ISBN :
0-7803-3274-1
Type :
conf
DOI :
10.1109/WESCON.1996.553963
Filename :
553963
Link To Document :
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