Eigenstructure assignment for design of multimode flight control systems
- 1 May 1985
- journal article
- Published by Institute of Electrical and Electronics Engineers (IEEE) in IEEE Control Systems Magazine
- Vol. 5 (2) , 9-15
- https://doi.org/10.1109/mcs.1985.1104941
Abstract
Advanced aircraft such as control configured vehicles (CCV) provide the capability for implementing multimode control laws, which allow the aircraft performance to be tailored to match the characteristics of a specific task or mission. This is accomplished by generating decoupled aircraft motions, which can be used to improve aircraft effectiveness. In this article, we describe a task-tailored multimode flight control system, which was designed by using eigenstructure assignment.Keywords
This publication has 4 references indexed in Scilit:
- A design methodology for pitch pointing flight control systemsJournal of Guidance, Control, and Dynamics, 1985
- Application of eigensystem assignment to lateral translation and yaw pointing flight controlPublished by Institute of Electrical and Electronics Engineers (IEEE) ,1984
- Eigenstructure Assignment for Linear SystemsIEEE Transactions on Aerospace and Electronic Systems, 1983
- The steady-state invertibility and feedforward control of linear time-invariant systemsIEEE Transactions on Automatic Control, 1976