@article{ref1,
title="A survey of force feedback in flight safety enhancement",
journal="Procedia engineering",
year="2012",
author="Wang, Junren and Pan, Xiang and Pan, Xue and Xue, Yali and Ye, Yongqiang",
volume="29",
number="",
pages="2303-2307",
abstract="This survey presents the application of force feedback in aviation. In modern fly-by-wire control system, actuator rate limit is the primary source of PIO II (Pilot Induced Oscillation II). The combination of smart-cue and smart-gain method can alleviate PIO II effectively, and consequently enhance the flight safety. The recent research of applying force feedback in aviation demonstrates that it is worthy of theoretical exploration and extensive utilization.<p />",
language="en",
issn="1877-7058",
doi="10.1016/j.proeng.2012.01.305",
url="http://dx.doi.org/10.1016/j.proeng.2012.01.305"
}