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High speed simulator: A simulator for all seasonsThe evolution of a high speed spacecraft simulator (HSS) is discussed from development and operations perspectives. The HSS is a series of simulators capable of modeling the spacecraft and its subsystems at different levels. The HSS was developed for the validation of the Galileo low gain antenna mission's flight software. Due to the successful performance of the HSS in assisting with the flight software validation, additional Galileo validation applications were identified. These applications include the modeling of other onboard data systems, such as the command and data subsystem and the attitude and articulation control subsystem. The HSS architecture, which consists of a number of components, is described and the operational use of the system is outlined.
Document ID
19970017098
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
Authors
Patel, K.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Reinholtz, W.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Robinson, W. J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Date Acquired
August 17, 2013
Publication Date
November 1, 1996
Publication Information
Publication: Proceedings of 4th International Symposium on Space Mission Operations and Ground Data Systems, volume 2
Volume: 2
Subject Category
Ground Support Systems And Facilities (Space)
Report/Patent Number
Paper SO96.5.02
Accession Number
97N19458
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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