Quadrotor attitude control method based on adaptive and non-fragile finite-time convergence
By adopting adaptive and non-fragile finite time convergence control methods on quadrotor drones, the problem of quadrotor quickly adjusting attitude in a short time is solved, achieving higher transient performance and rapid convergence capability.
Patent Information
- Application Number
- CN202411152792.4
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2024-08-21
- Publication Date
- 2025-03-28
- Estimated Expiration
- 2044-08-21
AI Technical Summary
During autonomous flight, it is difficult for the four-rotor drone to quickly adjust its attitude in a short time, resulting in insufficient transient performance, especially in emergency situations that cannot quickly converge to the set value.
Adaptive and non-frailty finite time convergence control method is adopted, and the mathematical model of the four-rotor is obtained, divided into position subsystem and attitude subsystem, and the controller is designed separately to suppress controller perturbation and improve transient performance.
While suppressing the disturbance of the controller, the controller is reduced due to physical and mechanical interference sensitivity, and the four-rotor is quickly and stably converging in a short time, improving transient performance.