Control of a Flapping-Wing Micro Air Vehicle: Sliding-Mode Approach

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Authors

Bluman, James E.
Kang, Chang-kwon
Shtessel, Yuri

Issue Date

2018

Type

journal-article

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Keywords

Aircraft Components and Structure , Aircraft Design , Aircraft Kinematics , Aircraft Operations

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Abstract

The realization of feasible flapping-wing micro air vehicles (FWMAVs) is hampered by many technical difficulties. In spite of these challenges, the natural world is full of successful designs that comprise a wide variety of sizes, shapes, and morphological features. For FWMAV developers, bumblebees are interesting because of their ability to hover, achieve high-speed forward flight, fly for long distances, carry heavy loads, maneuver adeptly, and maintain a hovering position in the face of significant wind gusts. However, several previous studies [1–5] have shown that flapping-wing insects possess an unstable mode, particularly for high-frequency flappers like bumblebees [4]. This unstable mode suggests the existence of an intrinsic flight instability of insects as well as the importance of feedback-based control of the wing kinematics for stable flight [6]...

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Citation

Control of a Flapping-Wing Micro Air Vehicle: Sliding-Mode Approach James E. Bluman, Chang-Kwon Kang, and Yuri Shtessel Journal of Guidance, Control, and Dynamics 2018 41:5, 1223-1226

Publisher

Aerospace Research Central

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PubMed ID

ISSN

0731-5090
1533-3884

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