A multi-dimensional approach has been carried out for design and development of a flapping
wing Ornithopter, used designing and analytic software including specific material for wings
and frame body of Ornithopter to produce lift and thrust for hovering and forward flight, by
considering the motion of a three-dimensional rigid thin wing in flapping and pitching motion
with phase lag. Salient features of specific mechanism aids to perfume better results compare
to other available models. Parametric study is carried out to reveal the aerodynamic
characteristics of ornithopter flight and for the analysis of various selected simple models in
the literature, to develop a flying ornithopter model. Further considerations have been given
to other important parameters such as flapping frequency and wing geometry for wellconceived
formulations with realistic and workable assumptions and limitations.

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