The use of a hybrid computer in the solution of trajectory optimization problems is described. The solution technique utilizes the indirect method and requires iterative computation of the initial condition vector of the co-state variables. Convergence of the iteration is assisted by feedback switching and contour modification. A simulation of the method in an on-line updating scheme is presented
The hybrid optimization techique for attitude control design is described in detail. The technque is...
The sensitivities of the convergence characteristics of the methods to initially assumed parameters ...
Solutions to trajectory optimization problems are carried out by the direct and indirect methods. Un...
Documentation of the NBODY trajectory optimization program is presented in the form of a mathematica...
Three numerical procedures for Mayer classical and non-classical problems in trajectory optimizatio
Digital and hybrid simulator computer programs for optimal control of satellite attitude maneuver
Perturbation method of computing optimum trajectories on hybrid and digital computer
Hybrid computer Monte Carlo method for optimization of systems containing random parameter
New methods to solve trajectory optimization problems are devised. The methods use direct transcript...
Trajectory optimization by direct descent to minimum cost using iterative computer solution
Dynamic programming and multistage decision processes in guidance, flight mechanics, and trajectory ...
In this paper, a hybrid methodology is used to determine optimal open loop controls for the atmosphe...
In this investigation, the automation of trajectory discretization, in the form of patch point place...
Perturbation method of trajectory optimization by fast time repetitive computations of state equatio...
This dissertation describes a hybrid optimization algorithm that is able to determine optimal trajec...
The hybrid optimization techique for attitude control design is described in detail. The technque is...
The sensitivities of the convergence characteristics of the methods to initially assumed parameters ...
Solutions to trajectory optimization problems are carried out by the direct and indirect methods. Un...
Documentation of the NBODY trajectory optimization program is presented in the form of a mathematica...
Three numerical procedures for Mayer classical and non-classical problems in trajectory optimizatio
Digital and hybrid simulator computer programs for optimal control of satellite attitude maneuver
Perturbation method of computing optimum trajectories on hybrid and digital computer
Hybrid computer Monte Carlo method for optimization of systems containing random parameter
New methods to solve trajectory optimization problems are devised. The methods use direct transcript...
Trajectory optimization by direct descent to minimum cost using iterative computer solution
Dynamic programming and multistage decision processes in guidance, flight mechanics, and trajectory ...
In this paper, a hybrid methodology is used to determine optimal open loop controls for the atmosphe...
In this investigation, the automation of trajectory discretization, in the form of patch point place...
Perturbation method of trajectory optimization by fast time repetitive computations of state equatio...
This dissertation describes a hybrid optimization algorithm that is able to determine optimal trajec...
The hybrid optimization techique for attitude control design is described in detail. The technque is...
The sensitivities of the convergence characteristics of the methods to initially assumed parameters ...
Solutions to trajectory optimization problems are carried out by the direct and indirect methods. Un...