Abstract The principle of active system control (ASC) can and should be applied at the elemental and modular levels of design of a system, as well as at the whole system level of design. 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 a dependency matrix structure with analysis of flight data, we present a rigorous model of flight mode detection. We also illustrate how the flight mode system works by providing examples of the program modules required.
Flight Mode Concept and Realisation
Active System Control ; 209-240
10.09.2017
32 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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