Abstract
A study adopts the disturbance-observer-based control scheme to enhance the flight control performance. This method is known as an active anti-disturbance strategy where the lumped disturbances from various sources are estimated by a disturbance observer (DO) and then incorporated into a nominal controller to compensate for their adverse effects. A preliminary study has demonstrated the disturbance rejection ability of this control strategy on a small-scale helicopter. The study proposes a novel disturbance-observer design that extends the scope of the classical one to a partial-state unmeasurable system.
Original language | English |
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Pages (from-to) | 2235-2240 |
Number of pages | 6 |
Journal | Journal of Guidance, Control, and Dynamics |
Volume | 38 |
Issue number | 11 |
DOIs | |
Publication status | Published - 2015 |
ASJC Scopus subject areas
- Control and Systems Engineering
- Aerospace Engineering
- Space and Planetary Science
- Electrical and Electronic Engineering
- Applied Mathematics