Add to ORKGLinear optimal control techniques used as synthesis tool to conceptually design control systems for large highly flexible launch vehicl
Analysis and synthesis techniques for linear systems and methods of minimizing sensitivity of optima...
Quasi-optimal control technique for space vehicle attitude, bounded acceleration rendezvous in free ...
Research dealt with the general area of optimal flight control synthesis for manned flight vehicles....
The application of optimal control technology to the design of a controller for the space shuttle de...
Application of quadratic optimal control, least squares state, and parameter estimation to stability...
Optimal sensitivity design techniques to design feedback control system for large, flexible booste
Mathematical model for determining minimax attitude control of aeroballistic launch vehicles - stabi...
The control of flexible spacecraft is a difficult problem because of large number of elastic modes; ...
Two problems are presented in the area of optimal control and its application to the design of attit...
Optimal control theory applied to piecewise constant approximation of large launch booster for first...
Variational calculus, gradient methods, maximum principle, and dynamic programing methods of optimal...
A new neighboring optimal control methodology is developed and applied to the fuel-optimal landing o...
Both feedback and feedforward control approaches for uncertain dynamical systems (in particular, wit...
In the design of a launch vehicle attitude control system two factors of major concern are the bendi...
An approach for an optimization-based integrated controls-structures design is presented for a class...
Analysis and synthesis techniques for linear systems and methods of minimizing sensitivity of optima...
Quasi-optimal control technique for space vehicle attitude, bounded acceleration rendezvous in free ...
Research dealt with the general area of optimal flight control synthesis for manned flight vehicles....
The application of optimal control technology to the design of a controller for the space shuttle de...
Application of quadratic optimal control, least squares state, and parameter estimation to stability...
Optimal sensitivity design techniques to design feedback control system for large, flexible booste
Mathematical model for determining minimax attitude control of aeroballistic launch vehicles - stabi...
The control of flexible spacecraft is a difficult problem because of large number of elastic modes; ...
Two problems are presented in the area of optimal control and its application to the design of attit...
Optimal control theory applied to piecewise constant approximation of large launch booster for first...
Variational calculus, gradient methods, maximum principle, and dynamic programing methods of optimal...
A new neighboring optimal control methodology is developed and applied to the fuel-optimal landing o...
Both feedback and feedforward control approaches for uncertain dynamical systems (in particular, wit...
In the design of a launch vehicle attitude control system two factors of major concern are the bendi...
An approach for an optimization-based integrated controls-structures design is presented for a class...
Analysis and synthesis techniques for linear systems and methods of minimizing sensitivity of optima...
Quasi-optimal control technique for space vehicle attitude, bounded acceleration rendezvous in free ...
Research dealt with the general area of optimal flight control synthesis for manned flight vehicles....