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Space shuttle rudder/speedbrake subsystem analysisThe Continuous System Modeling Program (CSMP) is described with its uses, its limitations, and its application to the rudder/speedbrake (R/SB) subsystem. The space shuttle R/SB is analyzed using the CSMP. Areas of analysis emphasized include: step response, ramp response, and the delay time or deadspace observed in system response. Results are presented and discussed.
Document ID
19760009051
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Duke, H. G. (Lockheed Electronics Co. Houston, TX, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1975
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
LEC-6730
NASA-CR-147415
JSC-09940
Report Number: LEC-6730
Report Number: NASA-CR-147415
Report Number: JSC-09940
Accession Number
76N16139
Funding Number(s)
CONTRACT_GRANT: NAS9-12200
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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