What is it about?
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.
Featured Image
Read the Original
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.
You can read the full text:
Contributors
The following have contributed to this page







