Design of attitude and rate command systems for helicopters using eigenstructure assignment
- 1 November 1989
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 12 (6) , 783-791
- https://doi.org/10.2514/3.20482
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- The LQG/LTR procedure for multivariable feedback control designIEEE Transactions on Automatic Control, 1987
- Influence of high-order dynamics on helicopter flight-control systembandwidthJournal of Guidance, Control, and Dynamics, 1986
- On the loop transfer recoveryInternational Journal of Control, 1986
- Design of an active flutter suppression systemJournal of Guidance, Control, and Dynamics, 1986
- Active flutter suppression using eigenspace and linear quadratic design techniquesJournal of Guidance, Control, and Dynamics, 1985
- Eigenstructure Assignment for Linear SystemsIEEE Transactions on Aerospace and Electronic Systems, 1983
- Multivariable feedback design: Concepts for a classical/modern synthesisIEEE Transactions on Automatic Control, 1981
- Robustness results in linear-quadratic Gaussian based multivariable control designsIEEE Transactions on Automatic Control, 1981
- On the flexibility offered by state feedback in multivariable systems beyond closed loop eigenvalue assignmentIEEE Transactions on Automatic Control, 1976
- Inclusion of Rotor Dynamics in Controller Design for HelicoptersJournal of Aircraft, 1973