Table of Contents
ISRN Mechanical Engineering
Volume 2011, Article ID 635815, 11 pages
Research Article

Actuator and Sensor Positioning Optimization in Control Design for a Large BWB Passenger Aircraft

Division of Control and Process Automation, Institute of Mechanics and Mechatronics, Vienna University of Technology, Wiedner Hauptstraße 8 / E325/A5, 1040 Vienna, Austria

Received 31 January 2011; Accepted 17 March 2011

Academic Editors: M. Ahmadian, D. Kalempa, and F. Liu

Copyright © 2011 A. Schirrer et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.


This paper states an approach to actuator and sensor positioning optimization and design in the control system design of a large blended wing body (BWB) passenger aircraft. Numerous objectives have to be achieved by the control system: loads alleviation, vibration attenuation, and the fulfillment of handling quality requirements. Exploiting the system structure and existing system knowledge (excitation, comfort, and load formulations), evaluation criteria are designed to assess actuator and sensor effectiveness and efficiency for the aircraft dynamic range of interest. The tasks of optimal actuator and sensor positioning, actuator sizing, and actuator bandwidth requirements are investigated, whereby solutions that are robust are sought with respect to parameter variations. The results are shown on a BWB passenger aircraft model and verified using a normalized closed-loop performance assessment approach.