Add to ORKGThis research describes and applies the recently introduced, general-purpose variable-time-domain ne...
Midcourse guidance analysis and optimization with discrete measurements for mission logic developmen
This research describes and applies the recently introduced, general-purpose variabletime-domain ne...
Dynamic programming and multistage decision processes in guidance, flight mechanics, and trajectory ...
Least squares optimum final value control method for determining steering angle program of rocket ve...
Determination of closed loop guidance function with linear, time-variable feedback studied by behavi...
Computer program constructs a sequence of optimal solutions to dynamically-approximate linear equati...
The optimization of spacecraft trajectories has been, and continues to be, critical for the developm...
The optimization of spacecraft trajectories has been, and continues to be, critical for the developm...
A regular perturbation analysis is presented. Closed-loop simulations were performed with a first or...
Midcourse maneuvers in interplanetary flight for flyby Jovian mission with spin stabilized spacecraf
Optimum time to apply single midcourse velocity correction and optimum schedule for corrections in v...
Entry guidance equations, reference trajectories, and guidance system mechanizatio
Three numerical procedures for Mayer classical and non-classical problems in trajectory optimizatio
Application of overall error or uncertainity in spacecraft trajectory determinations to define a tim...
This research describes and applies the recently introduced, general-purpose variable-time-domain ne...
Midcourse guidance analysis and optimization with discrete measurements for mission logic developmen
This research describes and applies the recently introduced, general-purpose variabletime-domain ne...
Dynamic programming and multistage decision processes in guidance, flight mechanics, and trajectory ...
Least squares optimum final value control method for determining steering angle program of rocket ve...
Determination of closed loop guidance function with linear, time-variable feedback studied by behavi...
Computer program constructs a sequence of optimal solutions to dynamically-approximate linear equati...
The optimization of spacecraft trajectories has been, and continues to be, critical for the developm...
The optimization of spacecraft trajectories has been, and continues to be, critical for the developm...
A regular perturbation analysis is presented. Closed-loop simulations were performed with a first or...
Midcourse maneuvers in interplanetary flight for flyby Jovian mission with spin stabilized spacecraf
Optimum time to apply single midcourse velocity correction and optimum schedule for corrections in v...
Entry guidance equations, reference trajectories, and guidance system mechanizatio
Three numerical procedures for Mayer classical and non-classical problems in trajectory optimizatio
Application of overall error or uncertainity in spacecraft trajectory determinations to define a tim...
This research describes and applies the recently introduced, general-purpose variable-time-domain ne...
Midcourse guidance analysis and optimization with discrete measurements for mission logic developmen
This research describes and applies the recently introduced, general-purpose variabletime-domain ne...