Abstract
This work proposes a kinematic nonlinear controller for an autonomous miniature helicopter that generates saturated reference velocity commands for accurate waypoint trajectory tracking. The control law design is based on a Lyapunov technique with a special choice of the system state equations using spherical coordinates. Stability of the control system is analyzed. Finally, simulation results are presented and discussed, which validate the proposed controller.
| Original language | English |
|---|---|
| Pages (from-to) | 856-870 |
| Number of pages | 15 |
| Journal | Asian Journal of Control |
| Volume | 16 |
| Issue number | 3 |
| DOIs | |
| Publication status | Published - 1 May 2014 |
Keywords
- helicopter
- Lyapunov
- nonlinear
- UAV
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