A system for controlling operation of an aircraft engine includes a master controller, a control node coupled to a component of the aircraft engine and to the master controller, wherein the control node includes a computing device for performing diagnosis of the component. The computing device is configured to assess performance of the component during operation of the aircraft, determine whether the component is performing within specification, and if not performing within specification, indicate that the component is out of specification.
Distributed control system with smart actuators and sensors
2016-11-01
Patent
Elektronische Ressource
Englisch
Active Control of Airframe Response with Distributed Smart Actuators
British Library Conference Proceedings | 2000
|Flutter Control Using Distributed Piezoceramic Actuators and Sensors
British Library Conference Proceedings | 1999
|A System Approach to Smart-Sensors and Smart-Actuators Design
SAE Technical Papers | 1988
|A system approach to smart-sensors and smart-actuators design
Kraftfahrwesen | 1988
|