Automatic aircraft landing control using nonlinear energy method
This paper presents the integration of longitudinal and lateral dynamics controller designed using Nonlinear Energy Method (NEM) for a research civil aircraft. This controller ensures the core attitudes of the aircraft such as roll, pitch, yaw and airspeed follows their reference value determined b...
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| Main Authors: | , , |
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| Format: | Conference or Workshop Item |
| Language: | English English |
| Published: |
IEEE
2010
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/5379/1/MSC2010_JN.pdf http://irep.iium.edu.my/5379/4/16296-Automatic_aircraft_landing_control_using_nonlinear_energy_method__SCOPUS.pdf http://irep.iium.edu.my/5379/ http://ieeexplore.ieee.org/xpls/abs_all.jsp?arnumber=5611294&tag=1 |
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