Methodologies for weight estimation of fixed and flapping wing micro air vehicles

M Hassanalian, A Abdelkefi - Meccanica, 2017 - Springer
One of the important steps in the sizing process of fixed and flapping wing micro air vehicles
(MAVs) is weight estimation of the electrical and structural components. In order to enhance …

The sticky-pad plane and other innovative concepts for perching uavs

M Anderson - 47th AIAA Aerospace Sciences Meeting Including The …, 2009 - arc.aiaa.org
MALL UAV's, also known as Micro Air Vehicles (MAVs) have recently shown much promise
in support of small combat units. Their small, man-packable size enables individual units to …

Plasma-based dynamic stall control and modeling on an aspect-ratio-one wing

T De Troyer, D Hasin, D Keisar, S Santra, D Greenblatt - AIAA Journal, 2022 - arc.aiaa.org
Quasi-static and dynamic stall control experiments, using dielectric barrier discharge plasma
actuators, were performed on a square-tipped aspect-ratio-one wing, with a NACA 0015 …

Increasing flight endurance of MAVs using multiple quantum well solar cells

M Hassanalian, M Radmanesh… - International Journal of …, 2014 - koreascience.kr
Abstract Micro Aerial Vehicles (MAVs) are useful devices to assess new features that may be
utilized in a full size aircraft to enhance performance or to increase endurance. In this article …

Effect of aspect ratio on aerodynamic characteristics at low Reynolds numbers

M Mizoguchi, H Itoh - AIAA journal, 2013 - arc.aiaa.org
The effect of the aspect ratio on the aerodynamic characteristics of rectangular wings is
experimentally investigated at Reynolds numbers on the order of 10 4. The aerodynamic …

Self-learned suppression of roll oscillations based on model-free reinforcement learning

Y Dong, Z Shi, K Chen, Z Yao - Aerospace Science and Technology, 2021 - Elsevier
The high-angle-of-attack uncommanded roll oscillations are dangerous and cause
significant challenges in flight control. This paper focuses on investigating the feasibility and …

ATLAS IV wing aerodynamic design: From conceptual approach to detailed optimization

SG Kontogiannis, DE Mazarakos… - Aerospace Science and …, 2016 - Elsevier
In this paper, the aerodynamic design of the ATLAS IV, remote controlled aircraft, is
summarized. A wing aerodynamic design methodology was established for a high lift-high …

[图书][B] Between Sea and Sky: Aerial Aquatic Locomotion in Miniature Robots

This book combines eight years of research in Aerial-Aquatic robotics and reflects upon the
progress made in this new domain from its beginnings at the Aerial Robotics Lab of Imperial …

Optimal aerodynamic design of airfoils in unsteady viscous flows

DN Srinath, S Mittal - Computer Methods in Applied Mechanics and …, 2010 - Elsevier
A continuous adjoint formulation is used to determine optimal airfoil shapes in unsteady
viscous flows at Re= 1× 104. The Reynolds number is based on the free-stream speed and …

On the birth of micro air vehicles

TJ Mueller - International Journal of Micro Air Vehicles, 2009 - journals.sagepub.com
The history of micro air vehicles really began with the development of model airplanes in the
19th century and the development of radio controlled model airplanes in the 20th century …