Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
721570 | IFAC Proceedings Volumes | 2007 | 6 Pages |
Abstract
Control allocation is useful for control of overactuated aerospace systems, and deals with distributing the total control demand among the individual actuators. Using control allocation, the actuator selection task is separated from the regulation task in the control design. We propose a novel control allocation algorithm that is based on n-dimensional interval bisection techniques. Application to a reusable launch vehicle is given.
Related Topics
Physical Sciences and Engineering
Engineering
Computational Mechanics