DESIGN AND EXPERIMENT OF A BIONIC FLAPPING WING MECHANISM WITH FLAPPING–TWIST–SWING MOTION BASED ON A SINGLE ROTATION

Design and experiment of a bionic flapping wing mechanism with flapping–twist–swing motion based on a single rotation

In the present study, a bionic SUNSCREEN LOTION SPF 40 flapping mechanism of a spatial six-bar configuration was designed to transform a single rotation of a motor into a three degrees of freedom “flapping–twist–swing” cooperative motion of a flapping wing.The kinematics model of the flapping mechanism movement was constructed.The flapping

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Numerical integration of the boundary value problems for the second order nonlinear ordinary differential equations of an arbitrary structure using an iterative procedure

An iterative procedure for numerical integration of boundary-value problems for nonlinear ordinary differential equations of the second order of arbitrary structure is suggested.The initial differential equation by algebraic transformation can be written as a linear inhomogeneous differential equation of the second order with constant coefficients;

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