"Proceeding American Control Conference, Seattle, WA, June 1986."Bibliography: p. 8.Research supported by General Electric Company. NASA Ames and Langley Research Centers grant NASA NAG2-297William H. Pfeil, Michael Athans, H. Austin Spang III
The state of the art of multivariable engine control is examined in order to determine future needs ...
Multivariable control theory is applied to the design of multiple input and output engine controls. ...
The development of control systems for jet engines requires a real-time computer simulation. The sim...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1984.MICROFIC...
This paper compares two previously published design procedures for two different multivariable contr...
A multivariable control design procedure based on the output feedback regulator formulation is descr...
Turbojet engines are becoming increasingly complex, with more control variables, to meet future dema...
Application of the Linear-Quadratic-Gaussian with Loop-Transfer-Recovery methodology to design of a ...
In this thesis the main theme is to demonstrate the potential performance improvements of gas turbin...
This is the final report on the research performed under NASA Glen grant NASA/NAG-3-1975 concerning ...
Small turboshaft engine control systems are traditionally single input single output (SISO) and are ...
Bibliography: leaf 8.NASA Ames and Langley Research Centers grant NASA/NAG-2-297by Armando A. Rodrig...
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...
"Proc. American Control Conference, Seattle, WA, June 1986."Bibliography: leaves 7-8.NASA Ames and L...
The state of the art of multivariable engine control is examined in order to determine future needs ...
Multivariable control theory is applied to the design of multiple input and output engine controls. ...
The development of control systems for jet engines requires a real-time computer simulation. The sim...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1984.MICROFIC...
This paper compares two previously published design procedures for two different multivariable contr...
A multivariable control design procedure based on the output feedback regulator formulation is descr...
Turbojet engines are becoming increasingly complex, with more control variables, to meet future dema...
Application of the Linear-Quadratic-Gaussian with Loop-Transfer-Recovery methodology to design of a ...
In this thesis the main theme is to demonstrate the potential performance improvements of gas turbin...
This is the final report on the research performed under NASA Glen grant NASA/NAG-3-1975 concerning ...
Small turboshaft engine control systems are traditionally single input single output (SISO) and are ...
Bibliography: leaf 8.NASA Ames and Langley Research Centers grant NASA/NAG-2-297by Armando A. Rodrig...
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...
"Proc. American Control Conference, Seattle, WA, June 1986."Bibliography: leaves 7-8.NASA Ames and L...
The state of the art of multivariable engine control is examined in order to determine future needs ...
Multivariable control theory is applied to the design of multiple input and output engine controls. ...
The development of control systems for jet engines requires a real-time computer simulation. The sim...
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