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
A general method for selection and optimization of trajectories.Space mission trajectory optimization by iterative minimizing of residual vector, using linear correction
Document ID
19660056613
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Campbell, J. H.
Moore, W. E.
Wolf, H.
Date Acquired
August 3, 2013
Publication Date
January 1, 1966
Subject Category
Space Sciences
Report/Patent Number
AIAA PAPER 65-697
Report Number: AIAA PAPER 65-697
Accession Number
66A35903
Funding Number(s)
CONTRACT_GRANT: NAS9-2527
Distribution Limits
Public
Copyright
Other
Keywords
SPACECRAFT TRAJECTORY
TRAJECTORY OPTIMIZATION
ITERATIVE SOLUTION

Available Downloads

There are no available downloads for this record.

Related Records

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