کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
808188 905680 2016 5 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Cicada (Tibicen linnei) steers by force vectoring
ترجمه فارسی عنوان
هدایت سیکادا (Tibicen linnei) توسط بردار نیرو
کلمات کلیدی
سیکادا؛ پرواز آزاد؛ بردار نیرو ؛ مانور هوایی؛ کنترل نیرو
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی مکانیک
چکیده انگلیسی


• Several free flights of cicada (Tibicen linnei) are studied (total of 42 wingbeats).
• Coordination between the aerodynamic force generation and change in flight path is investigated.
• Measurements and calculations show that the aerodynamic force is fixed to the body frame.
• Findings reveal that a simple force vectoring technique is used for steering all these flights.
• A similar strategy can be applied to the design of Micro Air Vehicles.

To change flight direction, flying animals modulate aerodynamic force either relative to their bodies to generate torque about the center of mass, or relative to the flight path to produce centripetal force that curves the trajectory. In employing the latter, the direction of aerodynamic force remains fixed in the body frame and rotations of the body redirect the force. While both aforementioned techniques are essential for flight, it is critical to investigate how an animal balances the two to achieve aerial locomotion. Here, we measured wing and body kinematics of cicada (Tibicen linnei) in free flight, including flight periods of both little and substantial body reorientations. It is found that cicadas employ a common force vectoring technique to execute all these flights. We show that the direction of the half-stroke averaged aerodynamic force relative to the body is independent of the body orientation, varying in a range of merely 20 deg. Despite directional limitation of the aerodynamic force, pitch and roll torque are generated by altering wing angle of attack and its mean position relative to the center of mass. This results in body rotations which redirect the wing force in the global frame and consequently change the flight trajectory.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Theoretical and Applied Mechanics Letters - Volume 6, Issue 2, March 2016, Pages 107–111
نویسندگان
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