NASA NTRS · 19910057048
Feedback linearization for control of air breathing engines
Abstract
The method of feedback linearization for control of the nonlinear nozzle and compressor components of an air breathing engine is presented. This method overcomes the need for a large number of scheduling variables and operating points to accurately model highly nonlinear plants. Feedback linearization also results in linear closed loop system performance simplifying subsequent control design. Feedback linearization is used for the nonlinear partial engine model and performance is verified through simulation.
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Phillips, Stephen, Mattern, Duane. 1991-06-01. Feedback linearization for control of air breathing engines. https://ntrs.nasa.gov/citations/19910057048
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