Event-Driven Robust Geometric Control for a Nano Unmanned Helicopter

This work presents the design of an event-driven position tracking control law for a nano unmanned helicopter with a body length less than 25 centimeters and a mass less than 70 grams. A robust geometric controller based on robust integral sign error (RISE) is devised to compensate for the unmanned helicopter’s modeling uncertainties as well as unknown external disturbances. An event-driven robust nonlinear control technique is formulated for the nano helicopter’s position loop control taking into account the very limited onboard computing resources of the nano unmanned helicopter. The stability of the helicopter’s closed-loop system is analyzed. And practical flying experiments are performed to verify the efficiency of the control method. The experimental results demonstrate that not only the tracking accuracy is guaranteed, but also the proposed control method can also successfully reduce the consumption of the onboard flight control unit’s computing resources.

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Publication Details

Journal
IEEE Transactions on Automation Science and Engineering
Published
2025-01-01
DOI
https://doi.org/10.1109/tase.2025.3559506
Primary Topic
Aerospace Engineering and Control Systems
Type
article
Field-Weighted Citation Impact
0.00
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article

Event-Driven Robust Geometric Control for a Nano Unmanned Helicopter

Bin Xian, Aochen Ma, Xun Gu
IEEE Transactions on Automation Science and Engineering
Aerospace Engineering and Control Systems
article

Event-Driven Robust Geometric Control for a Nano Unmanned Helicopter

Bin Xian, Aochen Ma, Xun Gu
article en

Abstract

This work presents the design of an event-driven position tracking control law for a nano unmanned helicopter with a body length less than 25 centimeters and a mass less than 70 grams. A robust geometric controller based on robust integral sign error (RISE) is devised to compensate for the unmanned helicopter’s modeling uncertainties as well as unknown external disturbances. An event-driven robust nonlinear control technique is formulated for the nano helicopter’s position loop control taking into account the very limited onboard computing resources of the nano unmanned helicopter. The stability of the helicopter’s closed-loop system is analyzed. And practical flying experiments are performed to verify the efficiency of the control method. The experimental results demonstrate that not only the tracking accuracy is guaranteed, but also the proposed control method can also successfully reduce the consumption of the onboard flight control unit’s computing resources.

IEEE Transactions on Automation Science and EngineeringVol. 22
Tianjin University (CN)
Affordable and clean energy
Openalex Percentile: Top 91%
Aerospace Engineering and Control Systems
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