Article ID Journal Published Year Pages File Type
721570 IFAC Proceedings Volumes 2007 6 Pages PDF
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