Civil aircraft design must be carried out in accordance with a large amount of airworthiness requirements. Failure to capture proper requirements in early design stage may lead to unnecessary design iterations and solution alternations. Therefore, a model based method is proposed for automatically mapping proper airworthiness requirements to a current design task in the early design. It mainly includes a design task model for formal representation of different aircraft features, and an airworthiness constraint model for semantically representing airworthiness regulations. Based on the study of model mapping rules, a searching algorithm is also developed to facilitate requirements acquisition. Finally, a software tool is also implemented using the above method and tested through a case study.
LIU Zelin
,
ZHANG Fang
. Model-based automatic capture of airworthiness requirements in civil aircraft design[J]. Science & Technology Review, 2019
, 37(7)
: 80
-87
.
DOI: 10.3981/j.issn.1000-7857.2019.07.012
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