@inproceedings{714bd053e9554daa859ba894badf3b3c,
title = "Reliable automatic landing control against actuator stuck faults",
abstract = "This paper presents a new LMI-based approach for developing reliable automatic landing controllers which can tolerate actuator stuck faults. The H2 control technique is used to guarantee tracking performance with respect to a given glide slope trajectory. A realistic fighter aircraft model is studied to illustrate the proposed approach. Nonlinear simulation under various faults and wind disturbances are included in this study. Simulation results show that the proposed reliable controller design approach can achieve zero steady-state tracking error, robustness against wind disturbances and reliability against actuator stuck faults.",
keywords = "Actuator stuck faults, Affine parameter-dependent lyapunov functions, Automatic landing, Reliable control",
author = "Fang Liao and Wang, {Jian Liang} and Poh, {Eng Kee} and Dong Li",
year = "2004",
doi = "10.2514/6.2004-5233",
language = "English",
isbn = "1563476703",
series = "Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
pages = "2283--2295",
booktitle = "Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference",
note = "Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference ; Conference date: 16-08-2004 Through 19-08-2004",
}