Decoupling and pole assignment in linear multivariable systems - A geometric approach
Decoupling and pole assignments in linear multivariable control systems using geometric method
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Decoupling and pole assignments in linear multivariable control systems using geometric method
Image orthicon in high precision astronomical camera, evaluating geometric accuracy and stability by distortion measurement
Geodetic parameters estimated from satellite dynamic and geometric solutions and Mariner 4 and 5 missions
Analytical investigation of effects of geometric changes on flow characteristics of tandem bladed compressor stators
Rotary spindle lathe attachments for machining geometrical cones
Gravimetric and geometric investigations with GEOS 1 and GEOS 2 - GEOS 2 conference
Flight test data on geometric, aerodynamic, and kinematic characteristics of two twin keel parawings during deployment
Calculation of near fields of reflector antennas by geometrical theory of diffraction
Mass spectroscopic determination of geometric isomers of alpha, beta-unsaturated carboxylic acids, noting various modes of fragmentation
Alpha-beta unsaturated carboxylic acids geometric isomers determination by mass spectroscopy
Numerical solution procedures evaluation for geometrically nonlinear structural analysis by direct stiffness method, noting capability of self correcting initial value formulation
Modified Newton-Raphson stiffness matrices and initial value formulations to geometrically nonlinear structural analysis for beam and plane stress triangular elements
IR spectral geometric albedos of Jupiter Galilean satellites, noting resemblance to spectra of frosts
A digital computer program known as SATANS (static and transient analysis, nonlinear, shells) for the geometrically nonlinear static and dynamic response of arbitrarily loaded shells of revolution is presented. Instructions for the preparation of the input data cards and other information necessary for the operation of the program are described in detail and two sample problems are included. The governing partial differential equations are based upon Sanders' nonlinear thin shell theory for the conditions of small strains and moderately small rotations. The governing equations are reduced to uncoupled sets of four linear, second order, partial differential equations in the meridional and time coordinates by expanding the dependent variables in a Fourier sine or cosine series in the circumferential coordinate and treating the nonlinear modal coupling terms as pseudo loads. The derivatives with respect to the meridional coordinate are approximated by central finite differences, and the displacement accelerations are approximated by the implicit Houbolt backward difference scheme with a constant time interval. The boundaries of the shell may be closed, free, fixed, or elastically restrained. The program is coded in the FORTRAN 4 language and is dimensioned to allow a maximum of 10 arbitrary Fourier harmonics and a maximum product of the total number of meridional stations and the total number of Fourier harmonics of 200. The program requires 155,000 bytes of core storage.
Differential geometric investigations of control problems with switched electrical networks
Genetic algorithms for function optimization employ genetic operators patterned after those observed in search strategies employed in natural adaptation. Two of these operators, crossover and inversion, are interpreted in terms of their algebraic and geometric properties. Stochastic models of the operators are developed which are employed in Monte Carlo simulations of their behavior.
After a general treatment of the gathering power of particle telescopes, exact formulae are presented for the geometrical factor and directional response of multielement cylindrically symmetric telescopes with circular or rectangular cross sections. Some useful approximations to these formulae are given. For the gathering power in arbitrary geometries, there is a discussion of applicable digital computer techniques focusing particularly on a Monte Carlo method.
This paper presents an assessment of the solution procedures available for the analysis of inelastic and/or large deflection structural behavior. A literature survey is given which summarized the contribution of other researchers in the analysis of structural problems exhibiting material nonlinearities and combined geometric-material nonlinearities. Attention is focused at evaluating the available computation and solution techniques. Each of the solution techniques is developed from a common equation of equilibrium in terms of pseudo forces. The solution procedures are applied to circular plates and shells of revolution in an attempt to compare and evaluate each with respect to computational accuracy, economy, and efficiency. Based on the numerical studies, observations and comments are made with regard to the accuracy and economy of each solution technique.