Add to ORKGDue to mass constraints aerospace systems tend to have lightweight and flexible structures leading t...
A method of synthesizing reduced-order optimal feedback control laws for a high-order system is deve...
This thesis presents a flight control law for the ascent phase of flight of the next generation of r...
Linear optimal control techniques used as synthesis tool to conceptually design control systems for ...
The application of optimal control technology to the design of a controller for the space shuttle de...
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; ...
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...
summary:This paper presents a novel robust optimal control approach for attitude stabilization of a ...
Control of distributed parameter systems and nonlinear systems is discussed with application to aero...
A study is made to develop controllers for the NASA-JSC Triangular Space Station and evaluate their ...
Application of spectral identification adaptive control system to large launch vehicle in complete c...
The objective of this contract was to develop mathematical algorithms for the integration of structu...
Due to mass constraints aerospace systems tend to have lightweight and flexible structures leading t...
A method of synthesizing reduced-order optimal feedback control laws for a high-order system is deve...
This thesis presents a flight control law for the ascent phase of flight of the next generation of r...
Linear optimal control techniques used as synthesis tool to conceptually design control systems for ...
The application of optimal control technology to the design of a controller for the space shuttle de...
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; ...
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...
summary:This paper presents a novel robust optimal control approach for attitude stabilization of a ...
Control of distributed parameter systems and nonlinear systems is discussed with application to aero...
A study is made to develop controllers for the NASA-JSC Triangular Space Station and evaluate their ...
Application of spectral identification adaptive control system to large launch vehicle in complete c...
The objective of this contract was to develop mathematical algorithms for the integration of structu...
Due to mass constraints aerospace systems tend to have lightweight and flexible structures leading t...
A method of synthesizing reduced-order optimal feedback control laws for a high-order system is deve...
This thesis presents a flight control law for the ascent phase of flight of the next generation of r...