High performance linear-quadratic and H-infinity designs for a 'supermaneuverable' aircraft
- 14 August 1989
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- The LQG/LTR procedure for multivariable feedback control designIEEE Transactions on Automatic Control, 1987