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Helicopter system identification is a challenging problem that requires systematic flight testing. We present a simple low complexity approach towards time domain system identification for helicopters which reduces the dependence on specific flight testing methods.

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This page is a summary of: Time-Domain System Identification of Helicopters Using Nonlinear Acceleration and Jerk Prediction Model, Journal of Aircraft, May 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c035273.
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