Design of Automatic Landing Systems Using Mixed H/H Control
- 1 January 1999
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 22 (1) , 103-114
- https://doi.org/10.2514/2.4356
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Aircraft Control and SimulationAircraft Engineering and Aerospace Technology, 2004
- Design of an autoland controller for an F-14 aircraft using H-infinity synthesisJournal of Guidance, Control, and Dynamics, 1996
- Mixed H2/H-infinity optimal control for an elastic aircraftJournal of Guidance, Control, and Dynamics, 1996
- H(2)/H9(infinity) controller design for a two-dimensional thin airfoil flutter suppressionJournal of Guidance, Control, and Dynamics, 1994
- Mixed ℋ/sub 2/ and ℋ/sub ∞/ performance objectives. II. Optimal controlIEEE Transactions on Automatic Control, 1994
- Mixed ℋ/sub 2/ and ℋ/sub ∞/ performance objectives. I. Robust performance analysisIEEE Transactions on Automatic Control, 1994
- Airport EngineeringPublished by Wiley ,1992
- Design of the flare control law for longitudinal autopilot using H/sub infinity / synthesisPublished by Institute of Electrical and Electronics Engineers (IEEE) ,1990