Publication Date:
2019-07-13
Description:
A framework was developed for the optimization and validation of empirical dynamic models subject to an arbitrary set of validation criteria. The validation requirements imposed upon the model, which may involve several sets of input-output data and arbitrary specifications in time and frequency domains, are used to determine if model predictions are within admissible error limits. The parameters of the empirical model are estimated by finding the parameter realization for which the smallest of the margins of requirement compliance is as large as possible. The uncertainty in the value of this estimate is characterized by studying the set of model parameters yielding predictions that comply with all the requirements. Strategies are presented for bounding this set, studying its dependence on admissible prediction error set by the analyst, and evaluating the sensitivity of the model predictions to parameter variations. This information is instrumental in characterizing uncertainty models used for evaluating the dynamic model at operating conditions differing from those used for its identification and validation. A practical example based on the short period dynamics of the F-16 is used for illustration.
Keywords:
Systems Analysis and Operations Research; Aircraft Stability and Control
Type:
AIAA Paper 2014-0608
,
NF1676L-16673
,
AIAA Guidance, Navigation, and Control Conference; Jan 13, 2014 - Jan 17, 2014; National Harbor, MD; United States
Format:
application/pdf
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