2021
DOI: 10.2514/1.j059621
|View full text |Cite
|
Sign up to set email alerts
|

Concurrent Design and Flight Mission Optimization of Morphing Airborne Wind Energy Wings

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1

Citation Types

0
4
0

Year Published

2021
2021
2023
2023

Publication Types

Select...
5
2

Relationship

3
4

Authors

Journals

citations
Cited by 7 publications
(4 citation statements)
references
References 38 publications
0
4
0
Order By: Relevance
“…In Figure 7 , the blue dash-dotted curve corresponds to the average fitness value f a , the black solid curve corresponds to the minimum fitness value f min , and finally the red dashed curve corresponds to f a − f min . Figure 7 illustrates that the diversity (measured by f a − f min ) decreases when SGA converges; thus, p c and p m should increase at early stage so as to increase the exploration capability ( Fasel et al, 2021 ). Nevertheless, extremely large values will counteract the algorithm converging to the global optimal ( Le Guisquet and Amabili, 2021 ).…”
Section: Methodsmentioning
confidence: 99%
“…In Figure 7 , the blue dash-dotted curve corresponds to the average fitness value f a , the black solid curve corresponds to the minimum fitness value f min , and finally the red dashed curve corresponds to f a − f min . Figure 7 illustrates that the diversity (measured by f a − f min ) decreases when SGA converges; thus, p c and p m should increase at early stage so as to increase the exploration capability ( Fasel et al, 2021 ). Nevertheless, extremely large values will counteract the algorithm converging to the global optimal ( Le Guisquet and Amabili, 2021 ).…”
Section: Methodsmentioning
confidence: 99%
“…These flexible aero-structures pose a considerable modeling challenge, as they involve highly coupled and nonlinear interactions between the aerodynamic and structural dynamics. A range of aeroelastic modeling methods exist, from high-fidelity models able to simulate the coupled fluid flow fields and the deformation of the wing structure (Goza & Colonius, 2017;Mittal & Iaccarino, 2005;Peskin, 2002), to controloriented data-driven models including viscous and unsteady effects (Brunton et al, 2013;Hemati et al, 2017;Hickner et al, 2022), and lower-fidelity models such as doublet-lattice methods (Albano & Rodden, 1969), strip theory (Kim et al, 2008), and panel methods (Fasel et al, 2021;Fonzi et al, 2020;Murua et al, 2012). These methods provide accurate models of aeroelastic effects; however, computationally more efficient models are often necessary for optimization and control, even at the expense of some fidelity.…”
Section: Statement Of Needmentioning
confidence: 99%
“…Shape transformation enables structures to drastically alter their 3D shape and, therefore, it enables the design of multi‐functional components that can adapt to different environmental conditions and operate more efficiently. For example, adaptive facades have been investigated for increasing the energy efficiency of buildings, [ 1 , 2 , 3 ] morphing wings for more efficient flight performance, [ 4 , 5 , 6 ] and highly packageable components for better transportation. [ 7 , 8 ] Despite significant advancements, for actual applications, most concepts lack needed functionalities.…”
Section: Introductionmentioning
confidence: 99%