NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
G and C boost and abort study summary, exhibit BA six degree of freedom simulation of rigid vehicles was developed to study space shuttle vehicle boost-abort guidance and control techniques. The simulation was described in detail as an all digital program and as a hybrid program. Only the digital simulation was implemented. The equations verified in the digital simulation were adapted for use in the hybrid simulation. Study results were obtained from four abort cases using the digital program.
Document ID
19720021013
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Backman, H. D.
(Boeing Co. Houston, TX, United States)
Date Acquired
August 6, 2013
Publication Date
June 30, 1972
Subject Category
Navigation
Report/Patent Number
NASA-CR-115714
REPT-5-2581-HOU-093
Report Number: NASA-CR-115714
Report Number: REPT-5-2581-HOU-093
Accession Number
72N28663
Funding Number(s)
CONTRACT_GRANT: NAS9-12183
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available