Add to ORKGMultivariable control theory is applied to the design of multiple input and output engine controls. Highly-accurate, real-time engine simulations are utilized for control development and checkout. Electro-optical control components are developed for use in electronic control systems having fiber optic data links. Integrated controls are developed for VSTOL and Rotorcraft propulsion systems. Post-stall models of engine systems are developed to aid in understanding and control of post-stall engine behavior
The major contribution of this research was the exposition of the fact that airframe and engine inte...
The workshop consisted of 24 technical presentations on various aspects of aircraft controls, rangin...
Accomplishments in applying Modern Control Theory to the design of controls for advanced aircraft tu...
The state of the art of multivariable engine control is examined in order to determine future needs ...
Discussed here is research at NASA Lewis in the area of propulsion controls as driven by trends in a...
The research needs in the area of propulsion control as driven by trends in advanced aircraft are co...
The benefits of linear quadratic regulator synthesis methods in designing a multivariable engine con...
As turbofan engines become more complex, the development of controls necessitate the use of multivar...
A multivariable control design for the F100 turbofan engine was evaluated, as part of the F100 multi...
Integration of propulsion and flight control systems and their optimization offers significant perfo...
The research vision of the NASA Lewis Research Center in the area of integrated flight and propulsio...
A multivariable control design procedure based on the output feedback regulator formulation is descr...
The need for a more sophisticated engine control system is discussed. The improvements in better thr...
The development of control systems for jet engines requires a real-time computer simulation. The sim...
This lecture will provide an overview of the aircraft turbine engine control research at NASA (Natio...
The major contribution of this research was the exposition of the fact that airframe and engine inte...
The workshop consisted of 24 technical presentations on various aspects of aircraft controls, rangin...
Accomplishments in applying Modern Control Theory to the design of controls for advanced aircraft tu...
The state of the art of multivariable engine control is examined in order to determine future needs ...
Discussed here is research at NASA Lewis in the area of propulsion controls as driven by trends in a...
The research needs in the area of propulsion control as driven by trends in advanced aircraft are co...
The benefits of linear quadratic regulator synthesis methods in designing a multivariable engine con...
As turbofan engines become more complex, the development of controls necessitate the use of multivar...
A multivariable control design for the F100 turbofan engine was evaluated, as part of the F100 multi...
Integration of propulsion and flight control systems and their optimization offers significant perfo...
The research vision of the NASA Lewis Research Center in the area of integrated flight and propulsio...
A multivariable control design procedure based on the output feedback regulator formulation is descr...
The need for a more sophisticated engine control system is discussed. The improvements in better thr...
The development of control systems for jet engines requires a real-time computer simulation. The sim...
This lecture will provide an overview of the aircraft turbine engine control research at NASA (Natio...
The major contribution of this research was the exposition of the fact that airframe and engine inte...
The workshop consisted of 24 technical presentations on various aspects of aircraft controls, rangin...
Accomplishments in applying Modern Control Theory to the design of controls for advanced aircraft tu...