Self-starting multistep methods for the numerical integration of ordinary differential equations
Self-starting multistep methods for numerical integration of ordinary differential equations
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Self-starting multistep methods for numerical integration of ordinary differential equations
Accumulation of errors using numerical integration methods for solving celestial equations of motion
Operational unification of finite difference methods for numerical integration of ordinary differential equations
Predictor-corrector algorithm applicable to numerical integration of satellite orbits in multirevolution steps
Numerical integration methods for computing flow of gas in chemical nonequilibrium behind normal shock wave
Cowell numerical integration and satellite orbit calculation
Numerical integration orbits and Brouwer and modified Brouwer orbits
Algorithm for use in estimating accumulated numerical integration errors
Digital simulation for error analysis of numerical integration schemes
Error growth and stability analyzed for numerical integration of differential equations in chemical kinetics
Numerical integration of coupled first order ODE OF greatly differing time constant
A comparison theorem estimating the difference between solutions of a perturbed and unperturbed equation is obtained. This is then applied to obtain error estimates in numerical integration problems, in particular, those problems involving computation of satellite orbits. The main result is a proof of the intuitive notion that the error in numerically integrating a stable equation grows less rapidly than for an unstable equation.
Difference methods for asymptotic estimates of errors at numerical integration of systems of ordinary differential equations
Application of group theory to numerical integration of motion equations of conservative dynamical system
Application of numerical integration procedures to restricted three-body problem
A self-starting, multistep procedure for the numerical integration of ordinary differential equations is devised to produce all the required backward differences directly from the initial equations. The self-starting element eliminates nonessential tallying to determine starting values.
Numerical integration techniques for real time digital flight simulation
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.