منابع مشابه
Resonance Based Flapping Wing Micro Air Vehicle
Flapping wing micro air vehicles have many possible applications and have therefore been the subject of extensive research. The Atalanta project aims to develop a fully autonomous, 10 cm wingspan, flapping wing sensor platform. The structure is based on a fully compliant resonating structure with passive wing pitching. Several design improvements have taken place since the last report. Introduc...
متن کاملNonlinear Aeroelastic Simulations of a Flapping Wing Micro Air Vehicle Using Two Unsteady Aerodynamic Formulations
Nonlinear aeroelasticity of a flapping wing Micro Air Vehicle (MAV) is analyzed in this paper. The geometrically nonlinear deformations are modeled by a nonlinear strain-based beam formulation, coupled with six rigid-body degrees of freedom of the aircraft. Wing flapping kinematics is described using a set of Euler angles. Two types of unsteady aerodynamic formulations are incorporated for load...
متن کاملModeling and Simulation Vehicle Air Brake System
Air brake system has been widely used in heavy trucks and intercity buses for its great superiority over other brake system. The practical performance of air brake system may be greatly different from if we analyze it with static theory. Thus, it is necessary to build an integrate air brake system model to simulate the process of brake accurately. However, the dynamic mathematic model of air br...
متن کاملModeling and Simulation of Nonlinear Dynamics of Flapping Wing Micro Air Vehicles
The derivation of the nonlinear dynamics of flapping wing micro air vehicles is presented. Simulation results investigate differences in the position and orientation of the body due to differing wing masses and aerodynamic modeling choices. The flapping wing micro air vehicle is modeled as a system of three rigid bodies: a body and two wings. Themass of the wings, and their associatedmass and i...
متن کاملKinematics Optimization for a Flapping-wing Micro Air Vehicle
A flight-dynamics oriented simulation model of a flapping-wing Micro Air Vehicle (MAV) has been developed. This concept is based on flapping flight performed in nature by insects or hummingbirds. An optimization of the flapping kinematics of the wing has been led, in order to maximize the mean lift and thus the payload. A neural network has been designed to reproduce the function shape of the w...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
ژورنال
عنوان ژورنال: International Conference on Aerospace Sciences and Aviation Technology
سال: 2017
ISSN: 2636-364X
DOI: 10.21608/asat.2017.22456