NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Iteration procedures for indirect trajectory optimization methods.Numerical method solution of nonlinear two point boundary value problem associated with optimum transfer of spacecraft
Document ID
19680040422
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Lewallen, J. M.
Tapley, B. D.
Williams, S. D.
Date Acquired
August 4, 2013
Publication Date
March 1, 1968
Publication Information
Publisher: JOURNAL OF SPACECRAFT AND ROCKETS, VOL. 5, P. 321-327. 10
Subject Category
Space Sciences
Report/Patent Number
AIAA PAPER 67-58
Report Number: AIAA PAPER 67-58
Meeting Information
Meeting: AEROSPACE SCIENCES MEETING
Location: NEW YORK, NY
Start Date: January 23, 1967
End Date: January 26, 1967
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
68A21394
Distribution Limits
Public
Copyright
Other

Available Downloads

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