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A method for determining optimal fixed-time, N-impulse trajectories between arbitrarily inclined orbits.Optimal fixed time N impulse trajectory determination between inclined orbits using primer vector theory method
Document ID
19680063320
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jezewski, D. J.
Date Acquired
August 4, 2013
Publication Date
October 1, 1968
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AND INTERNATIONAL ASTRONAUTICAL FEDERATION,
Subject Category
Space Sciences
Report/Patent Number
IAF PAPER AD-30
Report Number: IAF PAPER AD-30
Meeting Information
Meeting: CONGRESS OF THE INTERNATIONAL ASTRONAUTICAL FEDERATION
Location: NEW YORK, NY
Start Date: October 13, 1968
End Date: October 19, 1968
Accession Number
68A44292
Distribution Limits
Public
Copyright
Other

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