NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Saturn guidance conceptsFour approximations to closed loop steering function in application to spacecraft guidance
Document ID
19670021265
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Baker, C. D. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 3, 2013
Publication Date
January 1, 1967
Subject Category
Navigation
Accession Number
67N30594
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
APPROXIMATION METHOD
SPACECRAFT GUIDANCE
SATURN LAUNCH VEHICLE
Document Inquiry

Available Downloads

There are no available downloads for this record.

Related Records

IDRelationTitle19670021225Collected WorksResearch Achievements Reviews. Volume 1 - Series 1 Through 2219670021225Collected WorksResearch Achievements Reviews. Volume 1 - Series 1 Through 22N67-30554 17-34Collected Works
No Preview Available