Aeroservoelastic design optimization with experimental verification
2001 (English)In: Journal of Aircraft, ISSN 0021-8669, Vol. 38, no 5, 958-961 p.Article in journal (Refereed) Published
A demonstration of integrated design optimization of an aeroservoelastic system was presented. It was shown that the simultaneous design of structural and control system required a two-step procedure to result in a minimum weight design and a control law that is well-designed for all operating conditions. The essential dynamics was predicted using a aeroservoelastic model, and final design with 42% less weight penalty was obtained using the integrated approach.
Place, publisher, year, edition, pages
2001. Vol. 38, no 5, 958-961 p.
IdentifiersURN: urn:nbn:se:kth:diva-12429ISI: 000171526200025OAI: oai:DiVA.org:kth-12429DiVA: diva2:311472
QC 201004212010-04-212010-04-212011-02-08Bibliographically approved