Methods and apparatus for model predictive control of aircraft gas turbine engines

   
   

A method of designing the operations and controls of a aircraft gas turbine engine includes generating an operations model for the gas turbine include at least one objective function, defining operations and control constraints for the operations model of the gas turbine, and providing an online dynamic optimizer/controller that dynamically optimizes and controls operation of the gas turbine using model predictive control based on the operations model and the operations and control constraints using an Extended Kalman Filter for estimation.

 
Web www.patentalert.com

< IMAGE FORMING APPARATUS AND PROCESS CARTRIDGE INCLUDING A DEVELOPING DEVICE PROVIDED AT LEAST WITH A DEVELOPER HOLDING MEMBER FOR HOLDING A DEVELOPER CONTAINING A TONER AND A DEVELOPER REGULATING MEMBER

< Tool path planning process for component by layered manufacture

> Method and system for turbomachinery surge detection

> Eddy current data union

~ 00145