An Active Control Method of Structural Vibration Based on Non-probability Interval Confidence Reliability
A technology of structural vibration and active control, applied in the direction of non-electric variable control, electric controller, mechanical oscillation control, etc., can solve uncertainty and low reliability, damage stability, and will not improve the effective performance of the active control system, etc. problem, to achieve the effect of accurate calculation results
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[0212] During flight, especially at high speed and high altitude, the aircraft is easily subjected to vibration caused by airflow, which seriously affects the safety and service life of the aircraft. At the same time, because the structure of the aircraft is mainly flexible, with the continuous increase of the power of the aircraft power plant, the aircraft has experienced a relatively complex dynamic environment. As flexible accessories become larger and larger, the installation and use of lightweight flexible accessories will become a mainstream trend, and this change will bring about a very obvious change in characteristics. Due to the huge size of the light flexible, the proportion of the moment of inertia and mass in the whole system increases, making the impact of vibration on the system more obvious. The fundamental frequency of aircraft vibration caused by vibration is generally less than 2hz. At the same time, due to the small structural damping and long vibration att...
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