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A variable metric algorithm for constrained minimization based on an augmented Lagrangian
Author(s) -
Gruver W. A.,
Engersbach N. H.
Publication year - 1976
Publication title -
international journal for numerical methods in engineering
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 1.421
H-Index - 168
eISSN - 1097-0207
pISSN - 0029-5981
DOI - 10.1002/nme.1620100506
Subject(s) - augmented lagrangian method , mathematics , mathematical optimization , algorithm , lagrange multiplier , minification , constrained optimization
This paper concerns the implementation of a recent idea, attributed to Hestenes and Powell, based on solving the equality constrained finite dimensional minimization problem\documentclass{article}\pagestyle{empty}\begin{document}$$ \min \,\{ \,f(x)|(x)\, = \,0,\,x \in \,R^n \} $$\end{document}via the unconstrained problem\documentclass{article}\pagestyle{empty}\begin{document}$$ \min \,\{ f\,(x)\, + \, < g(x),\,\lambda > + 0.5 < g(x),\,Kg(x) > \,|\,x\, \in \,R^n,\,\lambda \, \in \,R^p $$\end{document}where ƒ is a non‐linear functional, g is a non‐linear mapping into R p , K is a prescribed matrix of penalty constants and λ is the Lagrange multiplier. The computational algorithm is based on restoring active constraints to first order and adjusting x in the remaining necessary conditions by gradient projection. The minimization is performed by the variable metric rank‐two BGFS update with linear search by cubic interpolation. Computational results using the algorithm include two problems of minimum fuel trajectory optimization—two impulse rendezvous with Comet Encke and three impulse constrained positioning of a geostationary satellite.

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