Add to ORKGOptimum time to apply single midcourse velocity correction and optimum schedule for corrections in variable time-of-arrival guidance - geometrical mode
The sensitivities of the convergence characteristics of the methods to initially assumed parameters ...
While continuing the application of the inverse dynamics approach in obtaining the optimal numerical...
Prediction of velocity requirements for minimum time response abort trajectories for midcourse guida...
Midcourse maneuvers in interplanetary flight for flyby Jovian mission with spin stabilized spacecraf
Dynamic programming applied to guidance correction for perturbed trajectory of spacecraf
This research describes and applies the recently introduced, general-purpose variabletime-domain ne...
Three numerical procedures for Mayer classical and non-classical problems in trajectory optimizatio
Algorithms and computation techniques for solving trajectory optimization problem
Midcourse guidance analysis and optimization with discrete measurements for mission logic developmen
Least squares optimum final value control method for determining steering angle program of rocket ve...
This research describes and applies the recently introduced, general-purpose variable-time-domain ne...
Maxima-minima theory, Pontryagin principle, and calculus of variations for optimal trajectory and co...
Reduced computer precision effect on midcourse navigation and guidance system using optimal filterin...
Determination of closed loop guidance function with linear, time-variable feedback studied by behavi...
Systems optimization for motion stability matrix problem - predictive guidance for Thor vehicle traj...
The sensitivities of the convergence characteristics of the methods to initially assumed parameters ...
While continuing the application of the inverse dynamics approach in obtaining the optimal numerical...
Prediction of velocity requirements for minimum time response abort trajectories for midcourse guida...
Midcourse maneuvers in interplanetary flight for flyby Jovian mission with spin stabilized spacecraf
Dynamic programming applied to guidance correction for perturbed trajectory of spacecraf
This research describes and applies the recently introduced, general-purpose variabletime-domain ne...
Three numerical procedures for Mayer classical and non-classical problems in trajectory optimizatio
Algorithms and computation techniques for solving trajectory optimization problem
Midcourse guidance analysis and optimization with discrete measurements for mission logic developmen
Least squares optimum final value control method for determining steering angle program of rocket ve...
This research describes and applies the recently introduced, general-purpose variable-time-domain ne...
Maxima-minima theory, Pontryagin principle, and calculus of variations for optimal trajectory and co...
Reduced computer precision effect on midcourse navigation and guidance system using optimal filterin...
Determination of closed loop guidance function with linear, time-variable feedback studied by behavi...
Systems optimization for motion stability matrix problem - predictive guidance for Thor vehicle traj...
The sensitivities of the convergence characteristics of the methods to initially assumed parameters ...
While continuing the application of the inverse dynamics approach in obtaining the optimal numerical...
Prediction of velocity requirements for minimum time response abort trajectories for midcourse guida...