NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Trajectory optimization using fast-time repetitive computation.Reentry trajectory optimization by repetitive computations of impulse response functions and state equations solution
Document ID
19670057343
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Raby, J. S.
Wingrove, R. C.
Date Acquired
August 3, 2013
Publication Date
January 1, 1966
Subject Category
Computers
Accession Number
67A36072
Distribution Limits
Public
Copyright
Other
Keywords
STATE EQUATION
COMPUTER METHOD
TRAJECTORY OPTIMIZATION
REENTRY TRAJECTORY

Available Downloads

There are no available downloads for this record.
No Preview Available