Real-Time Communication between Aero Gas Turbine Engine Controller and Pilot Online Monitoring System
Anupa.K1, Channabasappa Baligar2
1Anupa.K, B.E in E&CE from Visvesvaraya Technological University, Belgaum, Karnataka, India.
2Channabasappa Baligar, Member of Institute of Electronics & Telecommunication Engineers and member of Society of Electronics Engineers Belgaum, Karnataka, India.
Manuscript received on May 12, 2013. | Revised Manuscript received on June 13, 2013. | Manuscript published on June 30, 2013. | PP: 537-540 | Volume-2, Issue-5, June 2013. | Retrieval Number: E1881062513/2013©BEIESP
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© The Authors. Blue Eyes Intelligence Engineering and Sciences Publication (BEIESP). This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/)
Abstract: The application presented, is developed based on real-time systems which is built for a very small set of mission-critical applications like space craft’s , avionics and other distributed control systems. The modern software deals with external interfaces and has to consider various timing implications The platform is based on the VxWorks 5.4.2 and developed using Tornodo IDE 2.0.2 tool with the targeted deadline of 30 milliseconds at the baud rate of 9.6kbps. RS232 interface executes the role of Transportation and Communication, an interface cable used for serial communication between Digital Electronic Control Unit (DECU) and the host to transfer data to the pilot Online Monitoring System and that is based on Laboratory Virtual Instrument Engineering Workbench (LabVIEW )7.1.
Keywords: Aero gas turbine engine, Digital Electronic Control Unit (DECU), Online Monitoring display, RS232 serial communication.