Abstract
The nonlinear hover control of helicopter with parameter uncertainties was studied. In regard with it, the disturbance attenuation problem with internal stability for uncertain nonlinear systems was addressed. It was found that the six degree of freedom nonlinear controller designed for hovering helicopter could be exactly separated into three degree of freedom controllers, one for translational motion and the other for rotational motion.
| Original language | English |
|---|---|
| Pages (from-to) | 3454-3459 |
| Number of pages | 6 |
| Journal | Proceedings of the American Control Conference |
| Volume | 4 |
| Publication status | Published - 2003 |
| Event | 2003 American Control Conference - Denver, CO, United States Duration: 2003 Jun 4 → 2003 Jun 6 |
All Science Journal Classification (ASJC) codes
- Electrical and Electronic Engineering