Bistable Aerial Transformer: A Quadrotor Fixed-Wing Hybrid That Morphs Dynamically Via Passive Soft Mechanism

Author:

Weakly Jessica11,Li Xuan2,Agarwal Tejas33,Li Minchen456,Folk Spencer11,Jiang Chenfanfu22,Sung Cynthia1

Affiliation:

1. University of Pennsylvania Department of Mechanical Engineering, , Philadelphia, PA 19104

2. University of California, Los Angeles Department of Mathematics, , Los Angeles, CA 90095

3. University of Pennsylvania Department of Electrical Engineering, , Philadelphia, PA 19104

4. Carnegie Mellon University Department of Mathematics, , Los Angeles, CA 90095 ;

5. University of California, Los Angeles Department of Mathematics, , Los Angeles, CA 90095 ;

6. Carnegie Mellon University Computer Science Department, , Pittsburgh, PA 15213

Abstract

Abstract Aerial vehicle missions require navigating trade-offs during design, such as the range, speed, maneuverability, and size. Multi-modal aerial vehicles enable this trade-off to be negotiated during flight. This paper presents a Bistable Aerial Transformer (BAT) robot, a novel morphing hybrid aerial vehicle that switches between quadrotor and fixed-wing modes via rapid acceleration and without any additional actuation beyond those required for normal flight. The design features a compliant bistable mechanism made of thermoplastic polyurethane (TPU) that bears a large mass at the center of the robot’s body. When accelerating, inertial forces transition the vehicle between its stable modes, and a four-bar linkage connected to the bistable mechanism folds the vehicle’s wings in and out. The paper includes the full robot design and a comparison of the fabricated system to the elastodynamic simulation. Successful transitions between the two modes in mid-flight, as well as sustained flight in each mode indicate that the vehicle experiences higher agility in the quadrotor mode and higher flight efficiency in the fixed-wing mode, at an energy equivalent cost of only 2 s of flight time per pair of transitions. The vehicle demonstrates how compliant and bistable mechanisms can be integrated into future aerial vehicles for controllable self-reconfiguration for tasks such as surveillance and sampling that require a combination of maneuverability and long-distance flight.

Funder

National Science Foundation

Pennsylvania Space Grant Consortium

Publisher

ASME International

Reference57 articles.

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