T Feagin | University of Houston Clear Lake (original) (raw)

Uploads

Papers by T Feagin

Research paper thumbnail of Edge effects in lacunarity analysis

Ecological Modelling, 2007

Research paper thumbnail of Multistep methods of numerical integration using back-corrections

Celestial Mechanics & Dynamical Astronomy, 1976

A new class of linear multistep methods is proposed for the solution of the equations of motion o... more A new class of linear multistep methods is proposed for the solution of the equations of motion of certain dynamical systems encountered in celestial mechanics and astrodynamics. These methods are distinguished from the classical predictor-corrector methods in that they permit ‘back-corrections’ of the solution to be made. As the integration advances in time, the numerical solution is corrected or improved at certain points in the past. The enhanced numerical stability of these methods allows the meaningful application of high-order algorithms. Consequently, stepsizes larger than those attainable with the classical methods may be adopted and thus greater over-all efficiency may be realized. The application of these methods to the problem of determining the orbit of an artificial satellite is accomplished and the results are compared with those obtained using classical methods.

Research paper thumbnail of General perturbations on orbits with close encounters

Research paper thumbnail of Special perturbations using back-correction methods of numerical integration

A new class of linear multistep methods for numerical integration of differential equations is re... more A new class of linear multistep methods for numerical integration of differential equations is reported that permits satellite computation solutions to be corrected at certain points in the past as the integration advances in time. Algorithms have been developed for the solution of both first- and second-order differential equations. The back correction method appears to be more efficient than classical methods when dominant and perturbing forces can be separated.

Research paper thumbnail of A method of special perturbations using back corrections

Research paper thumbnail of The iterative solution of the problem of orbit determination using Chebyshev series

A method of orbit determination is investigated which employs Picard iteration and Chebyshev seri... more A method of orbit determination is investigated which employs Picard iteration and Chebyshev series. The method is applied to the problem of determining the orbit of an earth satellite from range and range-rate observations contaminated by noise. It is shown to be readily applicable and to possess linear convergence.

Research paper thumbnail of Edge effects in lacunarity analysis

Ecological Modelling, 2007

Research paper thumbnail of Multistep methods of numerical integration using back-corrections

Celestial Mechanics & Dynamical Astronomy, 1976

A new class of linear multistep methods is proposed for the solution of the equations of motion o... more A new class of linear multistep methods is proposed for the solution of the equations of motion of certain dynamical systems encountered in celestial mechanics and astrodynamics. These methods are distinguished from the classical predictor-corrector methods in that they permit ‘back-corrections’ of the solution to be made. As the integration advances in time, the numerical solution is corrected or improved at certain points in the past. The enhanced numerical stability of these methods allows the meaningful application of high-order algorithms. Consequently, stepsizes larger than those attainable with the classical methods may be adopted and thus greater over-all efficiency may be realized. The application of these methods to the problem of determining the orbit of an artificial satellite is accomplished and the results are compared with those obtained using classical methods.

Research paper thumbnail of General perturbations on orbits with close encounters

Research paper thumbnail of Special perturbations using back-correction methods of numerical integration

A new class of linear multistep methods for numerical integration of differential equations is re... more A new class of linear multistep methods for numerical integration of differential equations is reported that permits satellite computation solutions to be corrected at certain points in the past as the integration advances in time. Algorithms have been developed for the solution of both first- and second-order differential equations. The back correction method appears to be more efficient than classical methods when dominant and perturbing forces can be separated.

Research paper thumbnail of A method of special perturbations using back corrections

Research paper thumbnail of The iterative solution of the problem of orbit determination using Chebyshev series

A method of orbit determination is investigated which employs Picard iteration and Chebyshev seri... more A method of orbit determination is investigated which employs Picard iteration and Chebyshev series. The method is applied to the problem of determining the orbit of an earth satellite from range and range-rate observations contaminated by noise. It is shown to be readily applicable and to possess linear convergence.

Log In