Analytical redundancy methods

In order to achieve the project goals with a reliable avionics architecture the already installed sensor and actuator settings will be used in a novel to define input and output blending, as well as novel sensor and actuator fusion to provide fault tolerance. In addition, the challenging and open problem of optimal sensor/actuator selections is investigated in relation to the novel movables design. The document will describe the proposed FDIR and sensor-actuator selection methods and their application to the demonstrator aircraft configuration