Add to ORKGEffect of nonzero initial conditions on selection of minimax controllers for large launch vehicles and extremal bounded amplitude bounded rate inputs to linear system
This thesis constitutes a contribution to the theory of extremal control systems which come within t...
A nonlinear programming technique was developed for the automated design and optimization of autopil...
Quasi-optimal control technique for space vehicle attitude, bounded acceleration rendezvous in free ...
Optimal control theory applied to piecewise constant approximation of large launch booster for first...
Chebyshev minimax solutions for Saturn launch vehicle control problems, and hybrid-analog computer r...
Mathematical model for determining minimax attitude control of aeroballistic launch vehicles - stabi...
Variational calculus, gradient methods, maximum principle, and dynamic programing methods of optimal...
Fuel sloshing and rigid body oscillations in large rocket booster control during launchin
Time optimal control of linear systems with constraints on control amplitude and rat
The application of optimal control technology to the design of a controller for the space shuttle de...
Linear optimal control techniques used as synthesis tool to conceptually design control systems for ...
Application of quadratic optimal control, least squares state, and parameter estimation to stability...
Includes bibliographical references (p. 13-16).Status report; January 31, 1988Supported by NASA. NAG...
Optimal sensitivity design techniques to design feedback control system for large, flexible booste
"December 31, 1985."Bibliography: leaf 10.NASA Grant NSG 2-297 MIT OSP no. 95178Michael Athans, Gunt...
This thesis constitutes a contribution to the theory of extremal control systems which come within t...
A nonlinear programming technique was developed for the automated design and optimization of autopil...
Quasi-optimal control technique for space vehicle attitude, bounded acceleration rendezvous in free ...
Optimal control theory applied to piecewise constant approximation of large launch booster for first...
Chebyshev minimax solutions for Saturn launch vehicle control problems, and hybrid-analog computer r...
Mathematical model for determining minimax attitude control of aeroballistic launch vehicles - stabi...
Variational calculus, gradient methods, maximum principle, and dynamic programing methods of optimal...
Fuel sloshing and rigid body oscillations in large rocket booster control during launchin
Time optimal control of linear systems with constraints on control amplitude and rat
The application of optimal control technology to the design of a controller for the space shuttle de...
Linear optimal control techniques used as synthesis tool to conceptually design control systems for ...
Application of quadratic optimal control, least squares state, and parameter estimation to stability...
Includes bibliographical references (p. 13-16).Status report; January 31, 1988Supported by NASA. NAG...
Optimal sensitivity design techniques to design feedback control system for large, flexible booste
"December 31, 1985."Bibliography: leaf 10.NASA Grant NSG 2-297 MIT OSP no. 95178Michael Athans, Gunt...
This thesis constitutes a contribution to the theory of extremal control systems which come within t...
A nonlinear programming technique was developed for the automated design and optimization of autopil...
Quasi-optimal control technique for space vehicle attitude, bounded acceleration rendezvous in free ...