Simulation of EFIS system of Boeing 787 aircraft

Andreas Stefanidis Supervisor: Miroslav MacĂ­k Master thesis 2012
This work should be used to simulate Electronic Flight Instrument System (EFIS) of Boeing 787 aircraft. The solution will simulate various cockpit displays and will also implement the control panels to allow interaction with the EFIS. It will be also implemented an interface between EFIS and the platform which will provide simulation of the external environment and the physical model. The system will be designated for semi-professional use. In future, in the case of successful certification, it could be used for real flight crew training.