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Application of H 2 /H ∞ and dynamic inversion techniques to aircraft landing control
Aerospace Science and Technology
◽
10.1016/j.ast.2015.07.005
◽
2015
◽
Vol 46
◽
pp. 146-158
◽
Cited By ~ 19
Author(s):
Romulus Lungu
◽
Mihai Lungu
Keyword(s):
Dynamic Inversion
◽
Aircraft Landing
◽
Inversion Techniques
◽
Landing Control
Download Full-text
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References
Aircraft Landing Control Using the H-inf Control and the Dynamic Inversion Technique
Automation and Control Trends
◽
10.5772/62666
◽
2016
◽
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◽
Mihai Lungu
Keyword(s):
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◽
Inversion Technique
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Aircraft landing control in wind shear condition
2011 International Conference on Machine Learning and Cybernetics
◽
10.1109/icmlc.2011.6016885
◽
2011
◽
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Chia-Lin Lee
◽
Jih-Gau Juang
Keyword(s):
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◽
Aircraft Landing
◽
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◽
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The development of a total system aircraft landing control scheme
International Conference on Simulation (1998)
◽
10.1049/cp:19980634
◽
1998
◽
Cited By ~ 5
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Keyword(s):
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◽
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◽
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Application of generalised neural network for aircraft landing control system
Soft Computing
◽
10.1007/s00500-001-0159-1
◽
2002
◽
Vol 6
(6)
◽
pp. 441-448
◽
Cited By ~ 21
Author(s):
D. K. Chaturvedi
◽
R. Chauhan
◽
P. K. Kalra
Keyword(s):
Neural Network
◽
Control System
◽
Aircraft Landing
◽
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Aircraft Landing Control Based on CMAC and GA Techniques
IFAC Proceedings Volumes
◽
10.3182/20080706-5-kr-1001.01450
◽
2008
◽
Vol 41
(2)
◽
pp. 8576-8581
Author(s):
Wen-Pin Lin
◽
Jih-Gau Juang
Keyword(s):
Aircraft Landing
◽
Landing Control
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Automatic landing control using H-inf control and dynamic inversion
Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering
◽
10.1177/0954410014523576
◽
2014
◽
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◽
pp. 2612-2626
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Design of Carrier-Based Aircraft Landing Control Law Based on Direct Force
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◽
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◽
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◽
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Intelligent Fuzzy Systems for Aircraft Landing Control
Fuzzy Systems and Knowledge Discovery - Lecture Notes in Computer Science
◽
10.1007/11539506_105
◽
2005
◽
pp. 851-860
◽
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◽
Bo-Shian Lin
◽
Kuo-Chih Chin
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Fuzzy Systems
◽
Aircraft Landing
◽
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Aircraft landing control based on adaptive CMAC
2009 IEEE/ASME International Conference on Advanced Intelligent Mechatronics
◽
10.1109/aim.2009.5229913
◽
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◽
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◽
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◽
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Robust flight controller design using H-infinity loop-shaping and dynamic inversion techniques
10.2514/6.1998-4132
◽
1998
◽
Cited By ~ 4
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Martin Smit
◽
I. Craig
Keyword(s):
Controller Design
◽
Dynamic Inversion
◽
H Infinity
◽
Loop Shaping
◽
Inversion Techniques
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