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Optimal guidance with transition partial derivative matrices.Newton method for boundary value problem associated with differential equations applied to Lambert, rendezvous and orbital transfer problems
Document ID
19680063324
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ingram, H. L.
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-8
Report Number: IAF PAPER AD-8
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
68A44296
Distribution Limits
Public
Copyright
Other

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