Results 11 to 20 of about 256,703 (297)

Flight Performance Estimation of Bionic Flapping-Wing Micro Air Vehicle [PDF]

open access: yesXibei Gongye Daxue Xuebao, 2018
Bionic flapping-wing micro air vehicle(MAV) has received worldwide attention.The flight performance calculation is an important step in the conceptual design.The differences in performance estimation methods between the flapping-wing and conventional ...

doaj   +1 more source

Voice Operated Micro Air Vehicle [PDF]

open access: yesInternational Journal of Micro Air Vehicles, 2014
This paper presents the design of a Micro Air Vehicle (MAV) operated by speech commands. A person from a base station can comfortably control the motion of the MAV by issuing speech commands. This system proposes to have two units, one in the base station which is the control unit and the other is a flying machine.
P Sathish Kumar   +3 more
openaire   +1 more source

Micro Air Vehicle Nonlinear Simulation [PDF]

open access: yesInternational Conference on Aerospace Sciences and Aviation Technology, 2017
Micro air vehicle (MAV) is very sensitive to the external disturbances which make the prediction of its dynamics a hard task. In this paper there is a description of nonlinear simulation made for the MAV’s dynamics prediction. Experimental measured data were used in this Simulink simulation, the Aerodynamics forces and moment, Mass moment of inertia ...
Ahmed AboElezz   +3 more
openaire   +1 more source

Autonomous Door and Corridor Traversal with a 20-Gram Flapping Wing MAV by Onboard Stereo Vision

open access: yesAerospace, 2018
Autonomous flight of Flapping Wing Micro Air Vehicles (FWMAVs) is a major challenge in the field of robotics, due to their light weight and their flapping-induced body motions.
Sjoerd Tijmons   +3 more
doaj   +1 more source

Evaluation of the micro-carburetor [PDF]

open access: yes, 1981
A prototype sonic, variable-venturi automotive carburetor was evaluated for its effects on vehicle performance, fuel economy, and exhaust emissions.
Hall, R. A., Mazor, S. D., Weiss, M. F.
core   +2 more sources

Model identification of a Micro Air Vehicle [PDF]

open access: yesJournal of Bionic Engineering, 2007
This paper is focused on the model identification of a Micro Air Vehicle (MAV) in straight steady flight condition. The identification is based on input-output data collected from flight tests using both frequency and time domain techniques. The vehicle is an in-house 40 cm wingspan airplane.
Niño Castañeda, Jorge   +3 more
openaire   +2 more sources

Dynamic Stability and Flight Control of Biomimetic Flapping-Wing Micro Air Vehicle

open access: yesAerospace, 2021
This paper proposes an approach to analyze the dynamic stability and develop trajectory-tracking controllers for flapping-wing micro air vehicle (FWMAV). A multibody dynamics simulation framework coupled with a modified quasi-steady aerodynamic model was
Muhammad Yousaf Bhatti   +2 more
doaj   +1 more source

Optimization of the design of ducted-fan hovering micro air vehicles using finite element simulation and orthogonal design [PDF]

open access: yes, 2013
The structural design and flight stability characteristics of micro air vehicles have received much attention due to its low Reynolds number. Compared with fixed-wing aircraft, hovering ducted-fan micro air vehicles with vertical takeoff and landing and ...
Aono H   +16 more
core   +1 more source

Forceful manipulation with micro air vehicles

open access: yesScience Robotics, 2018
Micro air vehicles are able to anchor onto a surface within their environment and tug objects with up to 40 times their mass.
Matthew A. Estrada   +4 more
openaire   +2 more sources

Numerical Analysis of Bioinspired Tails in a Fixed-Wing Micro Air Vehicle

open access: yesAerospace, 2023
Bird tails play a key role in aerodynamics and flight stability. They produce extra lift for takeoff and landing maneuvers, enhance wing functions and maintain stability during flight (keeping the bird from yawing, rolling and pitching, or otherwise ...
Estela Barroso Barderas   +3 more
doaj   +1 more source

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