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

• URL: http://arxiv.org/abs/2604.22121v1
• Date: Thu, 23 Apr 2026 23:46:05 GMT
• Title: Characterizing pitch and roll torque coupling in insect-sized flapping-wing robots using a microfabricated gimbal
• Abstract summary: Coupling effects between roll and pitch torque actuation have not previously been measured.<n> microfabricated gimbal design capable of precisely and simultaneously measuring roll and pitch torques as well as thrust.<n>Results validate the assumption that pitch and toll can be considered independently in control.
• Score: 1.3955252961896318
• License: http://creativecommons.org/licenses/by-nc-sa/4.0/
• Abstract: Sub-gram flapping-wing flying insect robots (FIRs) are challenging to model because of mechanical complexity in their wings, unsteady aerodynamic flow, and the difficulty of making precise measurements at a small scale. Coupling effects between roll and pitch torque actuation have not previously been measured because a two-axis sensor that is sensitive enough has not been realized. To address this shortcoming, we introduce a microfabricated gimbal design capable of precisely and simultaneously measuring roll and pitch torques as well as thrust. We then used it to measure the extent to which a pitch torque command affects roll torque and vice versa on a 180 mg piezo-actuated flapping-wing flying platform. Our results show a high coefficient of determination in the linear regression for both pitch (0.95) and roll (0.98) and low cross-correlation coefficients (-0.001 and -0.085, respectively) across the full range of simultaneous torque commands, indicating negligible cross-axis coupling. Similarly, thrust force deviates by a maximum of only 5.8% from the mean thrust value. These results validate the assumption that pitch and toll can be considered independently in control and will inform future models of how inputs affect the aerodynamics of resonant flapping-wing systems.

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