Patent ID: 8814103
Filing Date: 2014-08-26
Classification: G05G

Abstract:
1. An aircraft control system comprising: a first feedback assembly movable relative to a mechanical ground; a first stick movable relative to the mechanical ground and the first feedback assembly, wherein: a) a first stick position is the position of the first stick relative to the mechanical ground; b) a first feedback position is the position of the first feedback assembly relative to the mechanical ground; and c) a first relative error is the first stick position minus the first feedback position; and a second feedback assembly movable relative to the mechanical ground; a second stick movable relative to the mechanical ground and the second feedback assembly, wherein: a) a second stick position is the position of the second stick relative to the mechanical ground; b) a second feedback position is the position of the second feedback assembly relative to the mechanical ground; and c) a second relative error is the second stick position minus the second feedback position; and