Analysis and comparison of several numerical optimization methods
Author:
Affiliation:
1. NASA, MANNED SPACECRAFT CENTER, HOUSTON, TEX.
2. TEXAS, U., AUSTIN, TEX.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1967-58
Reference21 articles.
1. Fig 4 illustrates the influence of the i n i t i a l iteration factor on convergence envelope size using a terminal time error of 0 percent. These envelopes are compiled from the previous three figures. Iterationscheme;Normal Initial iterationfactor: 1W% tl 1-11IIIIIII!!IIII111II tH
2. m
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2. Recurrent nature of Lagrange multipliers for optimal low-thrust earth-Jupiter transfers.;AIAA Journal;1969-07
3. Generation and measurement of high-amplitude square shocks in solids.;AIAA Journal;1968-05
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5. Comparison of several numerical optimization methods;Journal of Optimization Theory and Applications;1967-07
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