Results 21 to 30 of about 7,248 (202)

Study of a Flexible UAV Proprotor [PDF]

open access: yes, 2013
This paper is concerned with the evaluation of design techniques, both for the propulsive performance and for the structural behavior of a composite flexible proprotor.
Bénard, Emmanuel   +5 more
core   +2 more sources

Aerodynamic improvement of a delta wing in combination with leading edge flaps

open access: yesTheoretical and Applied Mechanics Letters, 2017
Recently, various studies of micro air vehicle (MAV) and unmanned air vehicle (UAV) have been reported from wide range points of view. The aim of this study is to research the aerodynamic improvement of delta wing in low Reynold’s number region to ...
Tadateru Ishide, Mao Itazawa
doaj   +1 more source

Position and Attitude Tracking of MAV Quadrotor Using SMC-Based Adaptive PID Controller

open access: yesDrones, 2022
A micro air vehicle (MAV) is physically lightweight, such that even a slight perturbation could affect its attitude and position tracking. To attain better autonomous flight system performance, MAVs require good control strategies to maintain their ...
Aminurrashid Noordin   +2 more
doaj   +1 more source

Propulsion for Biological Inspired Micro-Air Vehicles (MAVs)

open access: yesOpen Journal of Applied Sciences, 2016
Small Unmanned Aerial Vehicles have been receiving an increasingly interest in the last decades, fostered by the need of vehicles able to perform surveillance, communications relay links, ship decoys, and detection of biological, chemical, or nuclear materials. Smaller and handy vehicles Micro Air vehicles (MAVs) become even more challenging when DARPA
Jorge M. M. Barata   +3 more
openaire   +2 more sources

Development of a flapping mechanism inspired by the flexible wing-base structure of insects for wing motion control

open access: yesJournal of Biomechanical Science and Engineering, 2022
Flying insects are capable of hovering and rapid maneuver under unpredictable environments. The principal wing-beat is generated by transmitting the rhythmical contractions of power muscles to the exoskeleton and wing-base articulation.
Sakito KOIZUMI   +2 more
doaj   +1 more source

Flexibility Effects of a Flapping Mechanism Inspired by Insect Musculoskeletal System on Flight Performance

open access: yesFrontiers in Bioengineering and Biotechnology, 2021
Flying animals such as insects display great flight performances with high stability and maneuverability even under unpredictable disturbances in natural and man-made environments.
Sakito Koizumi   +2 more
doaj   +1 more source

Equilibrium transition study for a hybrid MAV [PDF]

open access: yes, 2011
Wind tunnel testing was performed on a VTOL aircraft in order to characterize longitudinal flight behavior during an equilibrium transition between vertical and horizontal flight modes.
Ameho, Yann   +3 more
core   +2 more sources

Design Optimization of a Micro Air Vehicle (MAV) Fixed Wing

open access: yesResearch Journal of Applied Sciences, Engineering and Technology, 2015
Micro air vehicles are gaining attention due to their wide range of applications in civilian and defense fields. The wings of these vehicles generate a particular flow regime which is to be explored further. Since the theories on the aerodynamics of all affects are still to be investigated, simulation based computational fluid dynamics is a good ...
D.V.A. Rama Sastry   +2 more
openaire   +1 more source

Fault-tolerant formation driving mechanism designed for heterogeneous MAVs-UGVs groups [PDF]

open access: yes, 2013
A fault-tolerant method for stabilization and navigation of 3D heterogeneous formations is proposed in this paper. The presented Model Predictive Control (MPC) based approach enables to deploy compact formations of closely cooperating autonomous aerial ...
A Abdessameud   +29 more
core   +1 more source

Propeller Slipstream Effect on Aerodynamic Characteristics of Micro Air Vehicle at Low Reynolds Number

open access: yesApplied Sciences, 2022
A numerical investigation on propeller-induced flow effects in tractor configurations on a Zimmerman wing-fuselage using the cambered thin airfoil is presented in this paper.
Zhaolin Chen, Fan Yang
doaj   +1 more source

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