Kinematic synthesis of flight control systems for light aircrafts
نویسندگان
چکیده
منابع مشابه
Optimal nonlinear control of flight faults in manned aircrafts in the presence of fault and failure of control actuato
Control actuators' faults are among the major reasons to lose aircraft control while flights. The plane dynamics is severely dependent upon faults and errors in flight control systems and if the reformed control order is not issued by the fault tolerant controller there would be unpleasant outcomes such as inconsistency and the reduction of system performance and some dreadful aerial accide...
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Publication of this report does not constitute approval by NASA of the findings or conclusions contained herein. It is published for the exchange and stimulation of ideas.
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ژورنال
عنوان ژورنال: Aircraft Engineering and Aerospace Technology
سال: 2002
ISSN: 0002-2667
DOI: 10.1108/00022660210414985