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PIO Engineering Prediction Methods and Verification of Airworthiness Compliance for Civil Aircraft
2019PIO (Pilot-Induced-Oscillation) is due to the mutual influence between abnormal aircraft response and pilot’s dynamic characteristic which causes the phenomenon that aircraft-pilot closed loop is instable. Therefore, airworthiness regulations (FAA25 CS25 CCAR25) 143 (a) (b) have given specific requirements for these.
Jun Liu, Nanbo Xu
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2010
A considerable amount of research effort has, and continues to be invested into technologies and algorithms for capabilities which are forecast to be needed in future uninhabited vehicles. Much of this research is conducted with the aim of increasing the level of autonomy of these vehicles.
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A considerable amount of research effort has, and continues to be invested into technologies and algorithms for capabilities which are forecast to be needed in future uninhabited vehicles. Much of this research is conducted with the aim of increasing the level of autonomy of these vehicles.
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An Airworthiness Compliance Verification Method for the Safety of Civil Aircraft IMA System
2021 International Conference on Aviation Safety and Information Technology, 2021Zhijian Shi, Zhen Feng
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Airworthiness Directives: Recovering the Cost of Compliance
Journal of Air Law and Commerce, 1984openaire +1 more source
Flap Design Optimization for Very Light Aircraft in compliance with Airworthiness Certification
21st AIAA Computational Fluid Dynamics Conference, 2013Jin-hwan Park +4 more
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Research on Ground Verification Technology of Civil Aircraft EWIS Airworthiness Compliance
2021openaire +1 more source