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Published on: March 10, 2011
Output feedback control of a quadrotor UAV using neural networks
Travis Dierks1, Sarangapani Jagannathan
1Department of Electrical and Computer Engineering, Missouri University of Science and Technology, Rolla, MO 65409, USA. tad5x4@mst.edu
A new nonlinear controller for quadrotor unmanned aerial vehicles (UAVs) uses neural networks (NNs) to learn dynamics online. This approach enables full six-degree-of-freedom control with only four inputs, improving stability and tracking.
Area of Science:
- Robotics
- Control Systems Engineering
- Artificial Intelligence
Background:
- Quadrotor unmanned aerial vehicles (UAVs) require sophisticated control strategies, especially in outdoor environments where dynamics are unpredictable.
- Traditional control methods often rely on accurate models of UAV dynamics, which are difficult to obtain in real-world scenarios.
- Underactuation in quadrotors limits control over all six degrees of freedom (DOF) using standard four-input configurations.
Purpose of the Study:
- To propose a novel nonlinear output feedback controller for quadrotor UAVs.
- To address the challenge of unknown and uncertain UAV dynamics by employing neural networks (NNs).
- To achieve simultaneous control of all six DOF despite the underactuated nature of the quadrotor.
Main Methods:
- An NN is utilized to learn the complete UAV dynamics online, including aerodynamic friction and blade flapping.
- A novel NN virtual control input scheme is developed to enable control of all six DOF from four inputs.
- An NN observer is introduced to estimate translational and angular velocities, with control laws based on measurable position and attitude.
Main Results:
- Lyapunov theory proves that position, orientation, and velocity tracking errors are semiglobally uniformly ultimately bounded (SGUUB).
- NN weight estimation errors and observer estimation errors are also shown to be SGUUB under bounded disturbances.
- The proposed controller effectively handles unknown nonlinear dynamics and disturbances, demonstrating robust performance.
Conclusions:
- The developed NN-based output feedback controller offers a robust solution for quadrotor UAV control with unknown dynamics.
- The method successfully overcomes the underactuation problem and achieves precise control of all six DOF.
- Simulation results validate the theoretical findings, confirming the effectiveness of the proposed control scheme.
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