MODELLING OF A FLAPPING-WING MICRO AERIAL VEHICLE
Publish place: 14th Annual Conference of Mechanical Engineering
Publish Year: 1385
نوع سند: مقاله کنفرانسی
زبان: English
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شناسه ملی سند علمی:
ISME14_549
تاریخ نمایه سازی: 1 فروردین 1386
Abstract:
This paper explores flapping flight as an effective form of locomotion for unmanned micro aerial vehicles (MAVs). In this paper a dynamic model of a flapping MAV is developed. We focus on a MAV with very limited wing kinematics and simple input control schemes. In particular, we parameterize wing trajectory based on biomimetic principles, i.e. principles that are directly inspired by observation of real insect flight. Flapping flight is analyzed from three different perspectives: biological, technological and control perspectives. Three specific aerodynamic effects are shown as the cause of a lift gain at low Re (Reynold’s number): the circulation generated by the rotation of the wing at the end of a stroke, the delayed stall due to the instationnarity of the movement, and finally the wake capture, as the wing re-enters the flow it has previously disturbed.
Keywords:
Flapping Flight– Micro Aerial Vehicles – Modelling – MAV
Authors
Bahram Tarvirdizadeh
Graduate Student, University of Tehran
Aghil Yousefi-Koma
Assistant Professor, University of Tehran
Esmaeel Khanmirza
Graduate Student, University of Tehran
Hesam maleki
Graduate Student, Civil organization of aviation
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