Design and testing of a high-specific work actuator using miniature pneumatic artificial muscles

Abstract

Micro-air vehicle (MAV) development is moving toward smaller and more capable platforms to enable missions such as indoor reconnaissance. This miniaturization creates challenging constraints on volume and energy generation/storage for all systems onboard. Actuator technologies must also address these miniaturization goals. Much research has focused on active material systems, such as piezoelectric materials and synthetic jets, but these advanced technologies have specific, but limited, capability. Conventional servo technology has also encountered concerns over miniaturization. Motivation has thus been established to develop a small-scale actuation technology prototype based on pneumatic artificial muscles, which are known for their lightweight, high-output, and low-pressure operation. The miniature actuator provides bidirectional control capabilities for a range of angles, rates, and loading conditions. Problems addressed include the scaling of the pneumatic actuators and design of a mechanism to adjust the kinematic load-stroke profile to suit the pneumatic actuators. The kinematics of the actuation system was modeled, and a number of bench-top configurations were fabricated, assembled, and experimentally characterized. Angular deflection and angular rate output of the final bench-top prototype system are presented, showing an improvement over conventional servo motors used in similar applications, especially in static or low-frequency operation.