Solution of variational problems by means of a generalized Newton-Raphson operator
Generalized Newton-Raphson operator for solving variational problems
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Generalized Newton-Raphson operator for solving variational problems
Algebraic matrix Riccati differential equation solution by Newton-Raphson iteration method
Solution of variational problems using newton- raphson operator
Computer program generates trajectories that are optimum with respect to payload placed in an earth orbit. It uses a subroutine package which produces the terminal and transversality conditions and their partial derivatives. This program is written in FORTRAN 4 and FORMAC for the IBM 7094 computer.
Time-optimal control theory applied to launch vehicle regulation and the newton-raphson optimization method
Numerical techniques for trajectory optimization discussing steepest descent, second variation and generalized newton-raphson methods
Steepest descent, second variation and generalized newton-raphson trajectory optimization techniques applied to minimum time, low thrust, circle-to- circle transfer problems
Computation of optimal interplanetary low thrust trajectories, orbital transfer problems by means of generalized Newton-Raphson method
Convergence proof and procedure for third-order and fourth-order iteration process for nonlinear equations - Newton-Raphson second-order iteration
Newton-Raphson method applied to solution of boundary value problems in trajectory optimization
Newton-Raphson method generalized for solution of two-point boundary value problems of nonlinear optimal control theory for digital solution
FORTRAN 2 computer program rapidly calculates parameters of maximum likelihood estimates from sensitivity experiment data populations. The program uses the Newton-Raphson iterative procedure to calculate the mean and standard deviation of portions of the cumulative normal response function.
Computer program synthesizes a passive network by minimizing the difference in desired and actual frequency response. The program solves for the critical points of the error function /weighted least squares fit between calculated and desired frequency response/ by the multivariable Newton-Raphson method with components constrained to an admissible region.
Computer program uses Bernoullis formula and Newton-Raphson method to provide steady state fluid flow analysis of line pressure drop in a system with six outlets for each of two main storage tanks. Program flexibility arises in the ease with which changes in the fluid line geometry can be made.
Program computes solutions for flow parameters in arbitrary gas mixtures behind a normal and a reflected normal shock, for in-flight and shock-tube stagnation conditions. Equilibrium flow calculations are made by a free-energy minimization technique coupled with the steady-flow conservation equations and a modified Newton-Raphson iterative scheme.
Quadratic Newton-Raphson iteration techniques for numerical solutions of Keplers universal transcendental equation
Low thrust trajectory optimization, using Newton- Raphson method to solve nonlinear two-point boundary value problem
Optimal free-space fixed thrust trajectories using impulsive trajectories as starting iteratives