Add to ORKGTwo problems are presented in the area of optimal control and its application to the design of attitude control systems for advanced complex aerospace vehicles. The problems discussed are specification of performance criteria in terms of structural load minimization and/or maximum orbital payload injection requirements of the controlled vehicle; and formulation and solution of the optimization problem such that practical control systems are obtained
Linear optimal control techniques used as synthesis tool to conceptually design control systems for ...
A collection of analytical studies is presented related to unconstrained and constrained aircraft (a...
Space vehicle, stochastic process, and bounded phase-coordinate process optimal control problems in ...
The hybrid optimization techique for attitude control design is described in detail. The technque is...
Variational calculus, gradient methods, maximum principle, and dynamic programing methods of optimal...
Mathematical model for determining minimax attitude control of aeroballistic launch vehicles - stabi...
Want to know not just what makes rockets go up but how to do it optimally? Optimal control theory ha...
Linear autonomous system theory and optimal control analysis for launch vehicle stability and antenn...
International audienceThis article surveys the classical techniques of nonlinear optimal control suc...
This dissertation develops a theoretical and practical framework for solving problems of optimal str...
The optimization technique is described which was used in the study for applying modern optimal cont...
The maximum-final mass trajectory of a proposed configuration of the Advanced Launch System is prese...
In the design of a launch vehicle attitude control system two factors of major concern are the bendi...
This thesis explores concepts for a closed-loop optimal control implementation of minimum-time attit...
The optimal control problem arising in coplanar orbital transfer employing aeroassist technology and...
Linear optimal control techniques used as synthesis tool to conceptually design control systems for ...
A collection of analytical studies is presented related to unconstrained and constrained aircraft (a...
Space vehicle, stochastic process, and bounded phase-coordinate process optimal control problems in ...
The hybrid optimization techique for attitude control design is described in detail. The technque is...
Variational calculus, gradient methods, maximum principle, and dynamic programing methods of optimal...
Mathematical model for determining minimax attitude control of aeroballistic launch vehicles - stabi...
Want to know not just what makes rockets go up but how to do it optimally? Optimal control theory ha...
Linear autonomous system theory and optimal control analysis for launch vehicle stability and antenn...
International audienceThis article surveys the classical techniques of nonlinear optimal control suc...
This dissertation develops a theoretical and practical framework for solving problems of optimal str...
The optimization technique is described which was used in the study for applying modern optimal cont...
The maximum-final mass trajectory of a proposed configuration of the Advanced Launch System is prese...
In the design of a launch vehicle attitude control system two factors of major concern are the bendi...
This thesis explores concepts for a closed-loop optimal control implementation of minimum-time attit...
The optimal control problem arising in coplanar orbital transfer employing aeroassist technology and...
Linear optimal control techniques used as synthesis tool to conceptually design control systems for ...
A collection of analytical studies is presented related to unconstrained and constrained aircraft (a...
Space vehicle, stochastic process, and bounded phase-coordinate process optimal control problems in ...