Diabatic and adiabatic representations for atomic collision problems.
Coupled equations for heavy particle motion expressed by introducing generalized matrix operator for effective momentum in atomic collision problems
Engineering topics
Publications and source records attributed to Smith, F. T..
Coupled equations for heavy particle motion expressed by introducing generalized matrix operator for effective momentum in atomic collision problems
Diatomic heavy particle collisions with emphasis on epithermal energy range, discussing elastic scattering and inelastic processes
Heavy particle spectroscopy, deducing collision parameters from empirical observations
Diatomic heavy particle collisions and elastic scattering and inelastic processes involving electronic excitation, ionization, and charge transfer or electronic energy
Atom-atom collision theory, comparing velocity criterion for inelastic scattering, Massey parameter and Landau-Zener parameter
Scaling law derived from small angle scattering theory, interpreting data in spectroscopic manner to deduce potentials and interactions between electronic states
Replotted data for elastic scattering of helium ions on neon and argon
Impact expansions and interference patterns in atomic scattering theory for cases of forward scattering, backscatter, inversion problem and screened Coulomb potential approximation
Perturbation effects in differential elastic ion- atom scattering generated by crossing of molecular states from even potentials
Elastic differential scattering in low energy helium ion collisions, discussing quantal and secondary interference and two-state theory
Nuclear symmetry effect on oscillations of elastic differential scattering of helium ion-atom resonant charge exchange
Spherically symmetrical classical scattering theory shows dependence on phase shift through appearance in quantal formulas for scattering amplitude and total cross section
Classical and quantal scattering - classical action
Optimization of 24-hour communication satellite orbital control process
Application of dynamic programming to optimizing the orbital control process of a 24-hour communications satellite
Description of a set of two-body orbital parameters useful for nearly circular orbits
Dynamic programming to optimize orbital control in a 24-hour communication satellite
Three-body problem - a symmetric representation - motion in a plane