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PIO Engineering Prediction Methods and Verification of Airworthiness Compliance for Civil Aircraft

open access: yes, 2019
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
openaire   +2 more sources
Some of the next articles are maybe not open access.

A Method for Airworthiness Compliance Verification of Minimum Flight Crew of Normal Category Aircraft

2024 12th International Conference on Information Systems and Computing Technology (ISCTech)
Hongni He, Zhi Ma
exaly   +2 more sources

Commercial Transport Aircraft Flight Simulator Flying Qualities Airworthiness Verification

Applied Mechanics and Materials, 2012
Flight 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
openaire   +1 more source

An Airworthiness Compliance Verification Method for the Safety of Civil Aircraft IMA System

2021 International Conference on Aviation Safety and Information Technology, 2021
Zhijian Shi, Zhen Feng
openaire   +1 more source

Taxiing stability verification and airworthiness certification for amphibious aircraft

Science China Information Sciences, 2018
Xufei He, Jianliang Ai
openaire   +1 more source

Safety and Airworthiness Verification of Civil Aircraft Engines

Journal of Mechanical Engineering and Technology, 2013
openaire   +1 more source

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