NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

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

Back to Results
Trajectory optimization program /TOP/.Steepest-ascent optimization program developed for flight path of current vehicles, particularly supersonic transport vehicles
Document ID
19670057229
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Matthews, M. L.
Stein, L. H.
Date Acquired
August 3, 2013
Publication Date
August 1, 1967
Subject Category
Navigation
Report/Patent Number
AIAA PAPER 67-561
Report Number: AIAA PAPER 67-561
Accession Number
67A35958
Funding Number(s)
CONTRACT_GRANT: NAS1-5293
Distribution Limits
Public
Copyright
Other
Keywords
COMPUTER PROGRAM
STEEPEST ASCENT METHOD
FLIGHT PATH
SUPERSONIC TRANSPORT
TRAJECTORY OPTIMIZATION
AIR BREATHING ENGINE

Available Downloads

There are no available downloads for this record.

Related Records

There are no records associated with this record.
No Preview Available