The artificial feel system can realize the simulation of helicopter control characteristics, which can be used for the test and evaluation of helicopter control system, and can also be used for flight quality research. Domestic research on artificial feel system has been carried out on fixed-wing variable-stability aircraft, but the research on helicopter is less. In this paper, the artificial feel system is studied from the following aspects: Introduction, design of the artificial feel system, assessment of space for artificial feel system, flight test, summary. The research results show that the artificial feel system functions normally, and the starting force characteristics and stick force gradient characteristics are variable.
Design and Flight Test of Artificial Feel System
Lect. Notes Electrical Eng.
International Conference on Man-Machine-Environment System Engineering ; 2023 ; Beijing, China October 20, 2023 - October 23, 2023
2023-09-05
8 pages
Article/Chapter (Book)
Electronic Resource
English
artificial feel system , flight test , starting force , stick force gradient Artificial Intelligence , Manufacturing, Machines, Tools, Processes , Environmental Engineering/Biotechnology , Engineering , Aerospace Technology and Astronautics , Engineering Economics, Organization, Logistics, Marketing
Longitudinal control feel system for in-flight research on response feel
Engineering Index Backfile | 1961
|Design of an Active Feel System for a Flight Simulator
SAE Technical Papers | 2000
|SAE Technical Papers | 2009
|