Robust flight control design using dynamic inversion and structured singular value synthesis
- 1 June 1993
- journal article
- Published by Institute of Electrical and Electronics Engineers (IEEE) in IEEE Transactions on Control Systems Technology
- Vol. 1 (2) , 80-92
- https://doi.org/10.1109/87.238401
Abstract
No abstract availableThis publication has 13 references indexed in Scilit:
- Automated gain schedules for missile autopilots using robustness theoryPublished by Institute of Electrical and Electronics Engineers (IEEE) ,2003
- A gain scheduled multivariable design for a manual flight control systemPublished by Institute of Electrical and Electronics Engineers (IEEE) ,2003
- Constrained control allocationJournal of Guidance, Control, and Dynamics, 1993
- A fixed H∞ controller for a supermaneuverable fighter performing the herbst maneuverAutomatica, 1993
- Gain scheduling: potential hazards and possible remediesIEEE Control Systems, 1992
- State-space solutions to standard H/sub 2/ and H/sub infinity / control problemsIEEE Transactions on Automatic Control, 1989
- State-space formulae for all stabilizing controllers that satisfy an H∞-norm bound and relations to relations to risk sensitivitySystems & Control Letters, 1988
- Flight control design using non-linear inverse dynamicsAutomatica, 1988
- All optimal Hankel-norm approximations of linear multivariable systems and theirL,∞-error bounds†International Journal of Control, 1984
- Analysis of feedback systems with structured uncertaintiesIEE Proceedings D Control Theory and Applications, 1982