Modeling and LQR control of insect sized flapping wing robot

Flying insects perform agile maneuvers like backflips, sharp turns, and collision recovery. Replicating these in sub-gram flying insect robots (FIRs) requires fast and responsive control systems. Current FIRs rely on elaborations of proportional-integral-derivative (PID)-type feedback control, requiring painstaking tuning and task-specific adjustments for complex maneuvers. Optimal control offers a solution but has been limited by approximate models or computational demands unsuitable for onboard implementation. Here, we used a more accurate stroke-averaged model of forces and torques, derived from a sensitive two-axis torque sensor, to implement the first demonstration of optimal control on an FIR that is computationally efficient enough to be performed by a microprocessor carried onboard. Applied to the 150 mg UW RoboFly, this enabled stable hovering (RMS error 2.5 cm) and trajectory tracking at speeds up to 25 cm/s using a linear quadratic regulator (LQR). These results were enabled by a more accurate model and laid the groundwork for integrating low-power receding-horizon control to achieve aggressive maneuvers in FIRs.

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Institutions

Publication Details

Journal
npj Robotics
Published
2025-03-19
DOI
https://doi.org/10.1038/s44182-025-00022-7
Citations
7
Primary Topic
Biomimetic flight and propulsion mechanisms
Type
article
Field-Weighted Citation Impact
34.95

Funders

Controls
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article

Modeling and LQR control of insect sized flapping wing robot

Kadierdan Kaheman, Daksh Dhingra, Sawyer B. Fuller
7 citations
npj Robotics
Biomimetic flight and propulsion mechanisms
34.95
article

Modeling and LQR control of insect sized flapping wing robot

Kadierdan Kaheman, Daksh Dhingra, Sawyer B. Fuller
article en
7 citations

Abstract

Flying insects perform agile maneuvers like backflips, sharp turns, and collision recovery. Replicating these in sub-gram flying insect robots (FIRs) requires fast and responsive control systems. Current FIRs rely on elaborations of proportional-integral-derivative (PID)-type feedback control, requiring painstaking tuning and task-specific adjustments for complex maneuvers. Optimal control offers a solution but has been limited by approximate models or computational demands unsuitable for onboard implementation. Here, we used a more accurate stroke-averaged model of forces and torques, derived from a sensitive two-axis torque sensor, to implement the first demonstration of optimal control on an FIR that is computationally efficient enough to be performed by a microprocessor carried onboard. Applied to the 150 mg UW RoboFly, this enabled stable hovering (RMS error 2.5 cm) and trajectory tracking at speeds up to 25 cm/s using a linear quadratic regulator (LQR). These results were enabled by a more accurate model and laid the groundwork for integrating low-power receding-horizon control to achieve aggressive maneuvers in FIRs.

npj RoboticsVol. 3(1)
University of Washington (US), Dolby (United States) (US)
National Science Foundation
Openalex Percentile: Top 0%
Biomimetic flight and propulsion mechanisms
34.95
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