Abstract
This paper addresses a new trajectory tracking controller for quad-rotor aircrafts in the presence of time-varying aerodynamic effect and bounded external disturbance using the novel script L1 adaptive control methodology augmented with nonlinear feed-forward compensations. The proposed augmented script L1 adaptive controller achieves uniformly bounded transient and asymptotic tracking of the output signal for any designated bounded reference trajectory. Finally, simulations of tracking a circular reference trajectory are performed to illustrate the validity of the proposed controller.
| Original language | English |
|---|---|
| Article number | 6978900 |
| Pages (from-to) | 3090-3101 |
| Number of pages | 12 |
| Journal | IEEE Transactions on Aerospace and Electronic Systems |
| Volume | 50 |
| Issue number | 4 |
| DOIs | |
| State | Published - 1 Oct 2014 |
Keywords
- Adaptation models
- Adaptive control
- Aerodynamics
- Rotors
- Trajectory
- Vectors
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