We describe a mockup for experimenting the control system design of an electrically actuated aircraft landing gear. The retraction and extension operations of the landing gear are modeled by a formal language and Petri nets are used to describe the control actions. Some ideas on how to manage possible temporary failures of some mechanical or electric components are also described
Some lab experiments on the control of an aircraft electrical landing gear / Garofalo, Francesco; Manzo, Ida. - (2014), pp. 228-231. (Intervento presentato al convegno 2014 International Symposium on Power Electronics, Electrical Drives, Automation and Motion tenutosi a Ischia, Italy nel 18 June 2014 -20 June 2014) [10.1109/SPEEDAM.2014.6871960].
Some lab experiments on the control of an aircraft electrical landing gear
GAROFALO, FRANCESCO;MANZO, IDA
2014
Abstract
We describe a mockup for experimenting the control system design of an electrically actuated aircraft landing gear. The retraction and extension operations of the landing gear are modeled by a formal language and Petri nets are used to describe the control actions. Some ideas on how to manage possible temporary failures of some mechanical or electric components are also describedI documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.
