Flight Envelope Expansion in Landing Phase Using Classic, Intelligent and Adaptive Controllers
- 1 January 2006
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 43 (1), 91-101
- https://doi.org/10.2514/1.13197
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- AUTOLANDING CONTROLLER DESIGN USING ADAPTIVE CONTROLPublished by World Scientific Pub Co Pte Ltd ,2004
- On the design of multivariable PID controllers via LMI approachAutomatica, 2002
- Neural networks as a tool for the assessment of human pilot behaviour in wind shearAerospace Science and Technology, 1999
- Design of Automatic Landing Systems Using Mixed H/H ControlJournal of Guidance, Control, and Dynamics, 1999
- An intelligent landing system based on a human skill modelIEEE Transactions on Aerospace and Electronic Systems, 1998
- Comprehensive analysis of two downburst-related aircraft accidentsJournal of Aircraft, 1996
- Design of the flare control law for longitudinal autopilot using H/sub infinity / synthesisPublished by Institute of Electrical and Electronics Engineers (IEEE) ,1990