Flight Mode: Concept and Realisation
摘要
Principle of active system control (ASC) can and should be applied at the element and module level of design of a system as well as at the system level. This chapter presents an application of ASC for flight mode determination using currently available flight data and the state of an aircraft (based on previous states of flight). Using dependency matrix structure with analysis of flight data we present a rigorous model of flight mode detection. We also illustrate how flight mode system works by providing examples of the program modules required.