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arxiv 2001.02320 v2 pith:3XK2MMAP submitted 2020-01-08 cs.RO cs.SYeess.SY

RoboFly: An insect-sized robot with simplified fabrication that is capable of flight, ground, and water surface locomotion

classification cs.RO cs.SYeess.SY
keywords flightrobotallowsdesigngroundlocomotionbecausecontrolled
verification ladder T0 review T1 audit T2 compute T3 formal T4 reserved
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Aerial robots the size of a honeybee (~100 mg) have advantages over larger robots because of their small size, low mass and low materials cost. Previous iterations have demonstrated controlled flight but were difficult to fabricate because they consisted of many separate parts assembled together. They also were unable to perform locomotion modes besides flight. This paper presents a new design of a 74 mg flapping-wing robot that dramatically reduces the number of parts and simplifies fabrication. It also has a lower center of mass, which allows the robot to additionally land without the need for long legs, even in case of unstable flight. Furthermore, we show that the new design allows for wing-driven ground and air-water interfacial locomotion, improving the versatility of the robot. Forward thrust is generated by increasing the speed of downstroke relative to the upstroke of the flapping wings. This also allows for steering. The ability to land and subsequently move along the ground allows the robot to negotiate extremely confined spaces, underneath obstacles, and to precise locations. We describe the new design in detail and present results demonstrating these capabilities, as well as hovering flight and controlled landing.

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Cited by 1 Pith paper

Reviewed papers in the Pith corpus that reference this work. Sorted by Pith novelty score.

  1. Characterizing pitch and roll torque coupling in insect-sized flapping-wing robots using a microfabricated gimbal

    eess.SY 2026-04 conditional novelty 7.0

    A new gimbal sensor shows negligible cross-coupling between pitch and roll torques on a piezo-actuated insect-sized flapping-wing robot, with linear responses and stable thrust.