NASA NTRS · 19770026221
Output feedback regulator design for jet engine control systems
Abstract
A multivariable control design procedure based on the output feedback regulator formulation is described and applied to turbofan engine model. Full order model dynamics, were incorporated in the example design. The effect of actuator dynamics on closed loop performance was investigaged. Also, the importance of turbine inlet temperature as an element of the dynamic feedback was studied. Step responses were given to indicate the improvement in system performance with this control. Calculation times for all experiments are given in CPU seconds for comparison purposes.
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Merrill, W. C.. 1977-01-01. Output feedback regulator design for jet engine control systems. https://ntrs.nasa.gov/citations/19770026221
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