Integral backstepping control for trajectory and yaw motion tracking of quadrotors

Author:

Poultney Alexander,Gong Peiyan,Ashrafiuon Hashem

Abstract

SUMMARYThis work presents a novel trajectory tracking, hovering, and yaw motion control for quadrotors subject to unknown modeling uncertainties and disturbances. Nonlinear equations of motion are used to model the quadrotor's motion without any simplifying assumptions. An integral backstepping control is developed by defining the tracking errors, their integral, and their first through third time derivatives as the system states. The resulting surge force and roll and pitch moments are shown to asymptotically stabilize the error states subject to bounded disturbances and modeling uncertainties. Similarly, a yaw moment is derived through integral backstepping that simultaneously stabilizes yaw motion errors. The controller performance in simultaneous trajectory and yaw motion tracking is verified through both simulations and experiments.

Publisher

Cambridge University Press (CUP)

Subject

Computer Science Applications,General Mathematics,Software,Control and Systems Engineering

Cited by 24 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Control design of quadrotor aircraft based on improved integral backstepping sliding mode;Asian Journal of Control;2024-07-03

2. Finite-Time Flight Control of a Quad-Copter UAV Using Integral Terminal Super-Twisting;2024 4th International Conference on Innovative Research in Applied Science, Engineering and Technology (IRASET);2024-05-16

3. Quantization Tracking Control Based on Disturbance Observer for the Unmanned Aerial Vehicles;2023 International Annual Conference on Complex Systems and Intelligent Science (CSIS-IAC);2023-10-20

4. Optimized FLPID using TLBO algorithm: Applied to Quadrotor (UAV) system;2023 International Conference on Advances in Electronics, Control and Communication Systems (ICAECCS);2023-03-06

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