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Adaptive robust tracking control of quadrotor helicopter with parametric uncertainty and external disturbance
- Source :
- 2017 International Conference on Unmanned Aircraft Systems (ICUAS).
- Publication Year :
- 2017
- Publisher :
- IEEE, 2017.
-
Abstract
- This paper proposes an adaptive robust tracking control strategy for a quadrotor helicopter with parametric uncertainties and external disturbances based on sliding mode control. The inner loop of the control strategy is concerned about the attitude and altitude control of the quadrotor helicopter, while the outer loop is employed to track the desired horizontal positions. By assuming knowledge of the bounds on external disturbances, an integral sliding mode control is designed to maintain system performance and keep it insensitive to disturbances. For parametric uncertainties (e.g., total mass and moments of inertia) of the quadrotor helicopter, an on-line adaptive scheme is proposed and incorporated into the nominal sliding mode control to deal with it. With this adaptive scheme, there is no need to know the parametric uncertainty bounds. A guaranteed transient and steady-state tracking performance can be obtained with the adaptive robust sliding mode controller. The effectiveness of the proposed control strategy is validated through a simulation on a quadrotor helicopter subject to parametric uncertainties and external disturbances.
- Subjects :
- 0209 industrial biotechnology
Engineering
business.industry
Control engineering
02 engineering and technology
Sliding mode control
Integral sliding mode
Computer Science::Robotics
020901 industrial engineering & automation
Computer Science::Systems and Control
Control theory
Robustness (computer science)
0202 electrical engineering, electronic engineering, information engineering
Torque
020201 artificial intelligence & image processing
Robust control
business
Inner loop
Parametric statistics
Subjects
Details
- Database :
- OpenAIRE
- Journal :
- 2017 International Conference on Unmanned Aircraft Systems (ICUAS)
- Accession number :
- edsair.doi...........f5826528d3dc88ee18ce2c7503e129ff
- Full Text :
- https://doi.org/10.1109/icuas.2017.7991398