Constrained minimization problems in finite- dimensional spaces.
Constrained minimization problems in finite- dimensional spaces in unified approach
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Constrained minimization problems in finite- dimensional spaces in unified approach
Constrained minimization problem extended to necessary conditions for characterizing noninferior points to determine vector-valued criteria in finite dimensional spaces
Conditions of optimality for constrained optimization problem
Constrained minimization under vector valued criteria in linear topological spaces
Constrained reliability optimization problems solution by integer programming noting parallel redundancy systems, formulation for standby redundant units and cost minimization
Second order necessary conditions of optimality for constrained optimization problems in finite dimensional spaces with vanished cost function gradient at optimal point
Computer analysis of nonlinear networks using constrained differential equations
Computation of regions of constrained stability for nonlinear control systems
Algorithm using gradient and restoration phases for constrained minimal problems
Integer programming method for optimizing constrained reliability problems with several system failure modes
Normalized hodographic mapping for constrained trajectory families, discussing mapping concepts, information content and applications
Stochastic differential games with constrained state estimators, involving linear system, quadratic cost functional and white Gaussian noises corrupting output measurements
Constrained complex optimization method for synthesizing distributed-lumped-active networks
Gyroscopic control of spin rate or orientation of rigid bodies constrained to rotate about fixed axis
Normalized hodographic mapping for constrained trajectory families, discussing mapping concepts, information content and applications
Description of a constrained split fairing technique for avoiding contamination of a sounding rocket's payload environment by an uncontained explosive actuation device. The development is presented of the equations of motion of the fairing halves during the opening sequence assumed to occur above the sensible atmosphere. It is believed that a significant insight into the general motion results from the solution obtained.
A linear shift-invariant preprocessing technique is described which requires no specific knowledge of the image parameters and which is sufficiently general to allow the effective radius of the composite imaging system to be minimized while constraining other system parameters to remain within specified limits.
For a time-dependent, n-dimensional, special diagonal Hamilton-Jacobi equation a necessary and sufficient condition for the separation of variables to yield a complete integral of the form was established by specifying the admissible forms in terms of arbitrary functions. A complete integral was then expressed in terms of these arbitrary functions and also the n irreducible constants. As an application of the results obtained for the two-dimensional Hamilton-Jacobi equation, analysis was made for a comparatively wide class of dynamical problems involving a particle moving in Euclidean three-dimensional space under the action of external forces but constrained on a moving surface. All the possible cases in which this equation had a complete integral of the form were obtained and these are tubulated for reference.