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PIO Engineering Prediction Methods and Verification of Airworthiness Compliance for Civil Aircraft
PIO (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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2024 12th International Conference on Information Systems and Computing Technology (ISCTech)
Hongni He, Zhi Ma
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Hongni He, Zhi Ma
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Commercial Transport Aircraft Flight Simulator Flying Qualities Airworthiness Verification
Applied Mechanics and Materials, 2012Flight simulation is a simulation of flight and various aspects of the flight environment. Flight simulation is used for a variety of reasons, including aircraft development and flight training. The engineering flight simulator is used for a certain commercial transport aircraft development.
Ya Ni Zhang, Yan Li, Ya Kui Gao
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Communications in Computer and Information Science
Yiyuan Zheng, Yuwen Jie, Shan Fu
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Yiyuan Zheng, Yuwen Jie, Shan Fu
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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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Taxiing stability verification and airworthiness certification for amphibious aircraft
Science China Information Sciences, 2018Xufei He, Jianliang Ai
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Safety and Airworthiness Verification of Civil Aircraft Engines
Journal of Mechanical Engineering and Technology, 2013openaire +1 more source
Research on Ground Verification Technology of Civil Aircraft EWIS Airworthiness Compliance
2021openaire +1 more source

