The basic feature of the optimisation-based clearance approach is to reformulate the clearance problems as equivalent minimum distance problems for which ”anti”-optimisation is performed to determine the worst-case parameter combination/ flight condition leading to worst performance. The basic requirements for the applicability of the optimisation-based approach are the availability of suitable parametric models describing the overall nonlinear dynamics of the augmented aircraft and of accompanying effcient and reliable trimming, linearisation and optimisation software tools. The optimisation-based approach has no limitations with respect to clearance criteria, being able to address all kind of clearance requirements which are expressible as mathematical criteria.
Optimisation-based clearance
2002-09-01
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
A Polynomial Based Clearance Method
AIAA | 2003
|Wiley | 2000
|Tema Archiv | 2009
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