| 摘要 |
<P>PROBLEM TO BE SOLVED: To provide an aircraft control system that provides tactile feedback between a plurality of control columns of the aircraft relating to discrepancies in the control inputs to the sticks of the respective control columns. <P>SOLUTION: The sticks 108, 110 each are coupled to an feedback assembly 112, 114 that is adjustable relative to mechanical ground 159 to adjust the feedback profile applied to the corresponding stick. The position of each feedback assembly is adjusted based on a relative displacement between the other feedback assembly and its corresponding stick to provide active feedback relating to the control of the other control column 102, 104. <P>COPYRIGHT: (C)2012,JPO&INPIT |
