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Aircraft Nonlinear Dynamic Instability Warning System
Aircraft Nonlinear Dynamic Instability Warning System
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机译:飞机非线性动态失稳预警系统
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摘要
A system and method for predicting aircraft nonlinear instability includes the steps of: (1) a pre-built aircraft state parameters for all possible flight conditions, (2) real time measuring flight parameters to determine aircraft state, (3) calculating the inertial coupling frequencies and periods as well as the nonlinear instability threshold based on the nonlinear instability theory recently developed by the inventor, (4) providing a first warning signal if the threshold is approached, (5) providing a second warning signal if the threshold has been exceeded.
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