| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 700422 | Control Engineering Practice | 2006 | 8 Pages |
Abstract
In this paper, a robust control scheme based on the quaternion feedback for attitude control of missiles employing thrust vector control is proposed. The control law consists of two parts: the nominal feedback part and an additional term for ensuring robustness to the plant uncertainties. For the proposed control scheme, a stability analysis is given and the performance is shown via computer simulation.
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Chanho Song, Sang-Jae Kim, Seung-Hwan Kim, H.S. Nam,