In the design of a launch vehicle attitude control system two factors of major concern are the bendi...
Elastic body equations in analysis and design of space vehicle flight control system
Fuel sloshing and rigid body oscillations in large rocket booster control during launchin
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...
Analysis and design of space vehicle control systems - short period dynamics of attitude control dur...
Mathematical analyses of suboptimal attitude maneuvering control for synchronous earth pointing sate...
Linear optimal control techniques used as synthesis tool to conceptually design control systems for ...
High power rockets could become dynamically unstable due to outside disturbances after takeoff. The ...
Application of quadratic optimal control, least squares state, and parameter estimation to stability...
This dissertation addresses Thrust Vector Control (TVC) design techniques for small launch vehicles ...
Variational calculus, gradient methods, maximum principle, and dynamic programing methods of optimal...
Absolute stability analysis of attitude control systems for large launch vehicle
Effect of nonzero initial conditions on selection of minimax controllers for large launch vehicles a...
This thesis presents a flight control law for the ascent phase of flight of the next generation of r...
In the design of a launch vehicle attitude control system two factors of major concern are the bendi...
Elastic body equations in analysis and design of space vehicle flight control system
Fuel sloshing and rigid body oscillations in large rocket booster control during launchin
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...
Analysis and design of space vehicle control systems - short period dynamics of attitude control dur...
Mathematical analyses of suboptimal attitude maneuvering control for synchronous earth pointing sate...
Linear optimal control techniques used as synthesis tool to conceptually design control systems for ...
High power rockets could become dynamically unstable due to outside disturbances after takeoff. The ...
Application of quadratic optimal control, least squares state, and parameter estimation to stability...
This dissertation addresses Thrust Vector Control (TVC) design techniques for small launch vehicles ...
Variational calculus, gradient methods, maximum principle, and dynamic programing methods of optimal...
Absolute stability analysis of attitude control systems for large launch vehicle
Effect of nonzero initial conditions on selection of minimax controllers for large launch vehicles a...
This thesis presents a flight control law for the ascent phase of flight of the next generation of r...
In the design of a launch vehicle attitude control system two factors of major concern are the bendi...
Elastic body equations in analysis and design of space vehicle flight control system
Fuel sloshing and rigid body oscillations in large rocket booster control during launchin
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