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Design and stable flight of a 21 g insect-like tailless flapping wing micro air vehicle with angular rates feedback control

An insect-like tailless flapping wing micro air vehicle (FW-MAV) without feedback control eventually becomes unstable after takeoff. Flying an insect-like tailless FW-MAV is more challenging than flying a bird-like tailed FW-MAV, due to the difference in control principles. This work introduces the...

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Published in:Bioinspiration & biomimetics 2017-04, Vol.12 (3), p.036006-036006
Main Authors: Phan, Hoang Vu, Kang, Taesam, Park, Hoon Cheol
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Language:English
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cited_by cdi_FETCH-LOGICAL-c367t-3277be78e122b133ede755dcabbdf339ae9df32ddac19524a416b1ea67180b233
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container_title Bioinspiration & biomimetics
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Kang, Taesam
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description An insect-like tailless flapping wing micro air vehicle (FW-MAV) without feedback control eventually becomes unstable after takeoff. Flying an insect-like tailless FW-MAV is more challenging than flying a bird-like tailed FW-MAV, due to the difference in control principles. This work introduces the design and controlled flight of an insect-like tailless FW-MAV, named KUBeetle. A combination of four-bar linkage and pulley-string mechanisms was used to develop a lightweight flapping mechanism that could achieve a high flapping amplitude of approximately 190°. Clap-and-flings at dorsal and ventral stroke reversals were implemented to enhance vertical force. In the absence of a control surface at the tail, adjustment of the location of the trailing edges at the wing roots to modulate the rotational angle of the wings was used to generate control moments for the attitude control. Measurements by a 6-axis load cell showed that the control mechanism produced reasonable pitch, roll and yaw moments according to the corresponding control inputs. The control mechanism was integrated with three sub-micro servos to realize the pitch, roll and yaw controls. A simple PD feedback controller was implemented for flight stability with an onboard microcontroller and a gyroscope that sensed the pitch, roll and yaw rates. Several flight tests demonstrated that the tailless KUBeetle could successfully perform a vertical climb, then hover and loiter within a 0.3 m ground radius with small variations in pitch and roll body angles.
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In the absence of a control surface at the tail, adjustment of the location of the trailing edges at the wing roots to modulate the rotational angle of the wings was used to generate control moments for the attitude control. Measurements by a 6-axis load cell showed that the control mechanism produced reasonable pitch, roll and yaw moments according to the corresponding control inputs. The control mechanism was integrated with three sub-micro servos to realize the pitch, roll and yaw controls. A simple PD feedback controller was implemented for flight stability with an onboard microcontroller and a gyroscope that sensed the pitch, roll and yaw rates. 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source IOPscience extra
subjects Air
Animals
Biomechanical Phenomena
Biomimetic Materials
biomimetics
Biomimetics - instrumentation
Coleoptera - anatomy & histology
Coleoptera - physiology
Efficiency
Equipment Design
flapping wing
Flight, Animal - physiology
hovering
insect flight
micro aerial vehicle (MAV)
Models, Biological
PD controller
Rotation
Wings, Animal - anatomy & histology
Wings, Animal - physiology
title Design and stable flight of a 21 g insect-like tailless flapping wing micro air vehicle with angular rates feedback control
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