Integrated uncertain optimal design strategy for truss configuration and attitude–vibration control in rigid–flexible coupling structure with interval uncertainties
By simultaneously considering the supported truss configuration optimization and optimal
attitude–vibration control in rigid–flexible coupling (RFC) structure, this study proposes a …
attitude–vibration control in rigid–flexible coupling (RFC) structure, this study proposes a …
Enhanced range and endurance evaluation of a camber morphing wing aircraft
BW Jo, T Majid - Biomimetics, 2023 - mdpi.com
Flight range, endurance, maneuverability, and agility are the key elements that determine an
aircraft's performance. Both conventional and morphing wing aircraft have been well studied …
aircraft's performance. Both conventional and morphing wing aircraft have been well studied …
Design and Control of an Ultra-Low-Cost Logistic Delivery Fixed-Wing UAV
Y Zhang, Q Zhao, P Mao, Q Bai, F Li, S Pavlova - Applied Sciences, 2024 - mdpi.com
In contemporary logistics, the deployment of fixed-wing unmanned aerial vehicles (UAVs) as
a transportation platform is experiencing rapid advancements, garnering substantial …
a transportation platform is experiencing rapid advancements, garnering substantial …
Comparative study of recent metaheuristics for solving a multiobjective transonic aeroelastic optimization of a composite wing
A transonic aeroelastic optimization approach for composite wing structure is proposed in
this study. Aerodynamic influence coefficient matrices are generated using doublet lattice …
this study. Aerodynamic influence coefficient matrices are generated using doublet lattice …