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Abstract
In this paper, flight guidance dynamics are shown to be implicit differentially flat with respect to the inertial position of an aircraft. This proves the existence of a set of relations between these flat outputs and the state variables representative of flight guidance dynamics and between these flat outputs and the basic inputs to flight guidance dynamics. A neural network is introduced to obtain, from the actual trajectory, nominal flight parameters which can be compared with actual values to detect abnormal behaviour.
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Published on 01/01/2007
Volume 2007, 2007
DOI: 10.1109/dasc.2006.313721
Licence: CC BY-NC-SA license
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