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A robust but easily implementable remote control for quadrotors: Experimental acrobatic flight tests

Published 3 Aug 2020 in eess.SY, cs.SY, and math.OC | (2008.00681v1)

Abstract: Experimental flight tests are reported about quadrotors UAVs via a recent model-free control (MFC) strategy, which is easily implementable. We show that it is possible to achieve acrobatic rate control of the UAV, which is beyond the previous standard. The same remote controller is tested on two physical vehicles without any re-tuning. It produces in both cases low tracking error. We show that MFC is robust even when the quadrotor is highly damaged. A video footage can be found at: https://youtu.be/wtSLalA4szc

Citations (11)

Summary

  • The paper presents a model-free control approach that robustly enables acrobatic quadrotor maneuvers without explicit system modeling.
  • The authors experimentally validate the method on multiple UAV platforms, including standard and modified configurations, achieving minimal tracking error.
  • Comparative analyses reveal that the MFC strategy outperforms PID control in adaptability and stability, offering significant practical benefits.

Analysis of Model-Free Control Application in Quadrotor UAVs

The paper "A robust but easily implementable remote control for quadrotors: Experimental acrobatic flight tests" presents a study on the application of a Model-Free Control (MFC) strategy in controlling quadrotor Unmanned Aerial Vehicles (UAVs). The research focuses on demonstrating the robustness and ease of implementation of MFC, specifically in acrobatic flight scenarios that extend beyond traditional control challenges.

Overview of Methodology and Approach

Model-Free Control, as explored in this research, offers a significant departure from conventional PID controllers by eschewing the need for explicit modeling of system dynamics. The MFC approach, derived from an ultra-local model underpins its operations by maintaining an adaptable control loop that accounts for both unmodeled dynamics and external disturbances. The ultra-local model simplifies the dynamics of a SISO system into a form that allows for straightforward control via estimated feedback.

Experimental Validation and Observations

The experimental section of the study details the trials conducted with MFC applied to different quadrotor configurations. This section reports implementations on multiple distinct UAV platforms with consistent success without re-tuning the controller parameters. Two specific scenarios underscore MFC's robustness:

  • Implementation on a standard DJI F450 frame that achieved minimum error in reference tracking during acrobatic maneuvers.
  • A highly compromised version of the same UAV, with damaged propellers, showcased MFC's resilience in maintaining flight controllability under modified dynamics, indicating significant robustness.

Additionally, a new quadrotor model, the Tarot 650 Sport, was employed to confirm MFC's adaptability across different vehicle dynamics. During these tests, it was observed that MFC maintained control effectiveness, despite changing vehicle dynamics and unintentional imbalance in the landing gear.

Comparative Analysis with PID Control

The paper goes further to compare MFC with conventional PID control. It highlights the inadequacies of PID when transitioning between different UAV platforms without re-tuning. This comparative analysis was demonstrated through the control performance of Tarot and F450 under PID control, revealing that MFC offered superior stability and control accuracy.

Implications and Future Directions

The implementation of MFC presents a low-cost and computationally efficient alternative to traditional control systems, with a direct impact on the design and functionality of UAVs in dynamic and volatile environments. The system's robustness, coupled with its low computational overhead, makes it highly suitable for deployment on both micro and macro UAV systems.

Practically, the MFC's utility in maintaining flight stability despite changes in system dynamics has implications for defense and emergency response scenarios where UAVs are subject to unexpected perturbations or damage. Theoretically, it opens avenues for exploring control strategies that do not rely on precise mathematical models of the system, thus broadening the scope for adaptive and resilient autonomous systems.

The ongoing research agenda includes expanding MFC to encompass additional degrees of freedom such as altitude and spatial navigation, thereby broadening the controller's applicability to comprehensive UAV control. Additionally, integration with GPS and barometric inputs is proposed to enhance navigational accuracy and control depth.

In conclusion, the research underlines Model-Free Control as a viable technique for quadrotor UAVs, achieving robust control without extensive system modeling. This approach not only supports but potentially transforms UAV operational paradigms, particularly in settings requiring robust and adaptable control solutions.

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