DocumentCode
332534
Title
Implementation and testing of International Space Station flight software for the pointing and support portion of guidance, navigation and control
Author
Yazell, Douglas J.
Author_Institution
Commercial Syst. Oper., Honeywell Space Syst., Houston, TX, USA
Volume
1
fYear
1998
fDate
31 Oct-7 Nov 1998
Abstract
Boeing engineers designed and implemented these algorithms using MOODS (Multibody On-Orbit Dynamics Simulation), a Boeing/NASA Ada non-realtime simulation running on a DEC Alpha platform in Boeing Tower 2 in Houston, Texas. The Ada flight software was then written in MatrixX superblocks on Hewlett Packard computers, using the MatrixX autocode capability to generate the Ada code. After Flight Stage 5A of the International Space Station (ISS), the Pointing and Support (P&S) subsystem is activated and provides the Guidance, Navigation, and Control (GN&C) interface for most of the other U.S. subsystems. P&S supplies state vector (ISS position and velocity), attitude, and attitude rate data to other ISS systems
Keywords
aerospace simulation; aerospace testing; attitude control; program testing; space vehicles; Ada nonrealtime simulation; DEC Alpha platform; International Space Station flight software; MOODS; MatrixX autocode capability; MatrixX superblocks; attitude rate data; guidance; multibody on-orbit dynamics simulation; navigation; pointing; space vehicle control; state vector; support portion; Aerospace engineering; Algorithm design and analysis; Automatic programming; Computational modeling; Design engineering; International Space Station; Mood; NASA; Poles and towers; Testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference, 1998. Proceedings., 17th DASC. The AIAA/IEEE/SAE
Conference_Location
Bellevue, WA
Print_ISBN
0-7803-5086-3
Type
conf
DOI
10.1109/DASC.1998.741486
Filename
741486
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