A New Algorithm on Automatic Trimming for Helicopter Rotor Aerodynamic Loads

In order to simulate the flight state of the helicopter effectively, it is necessary to trim the helicopter during the forward flight in a wind tunnel test. Previously, due to the lack of an internal-control closed loop in the test rig, the helicopter-wind-tunnel-test trimming was carried out manual...

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Bibliographic Details
Main Authors: Xinfan Yin, Hongxu Ma, Xianmin Peng, Guichuan Zhang, Honglei An, Liangquan Wang
Format: Article
Language:English
Published: MDPI AG 2023-02-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/10/2/150