发明名称 Altitude and acceleration command altitude hold algorithm for rotorcraft with large center of gravity range
摘要 A flight control system includes an Acceleration and Attitude Command/Velocity Hold mode (AACVH) algorithm which blends attitude commands with acceleration commands. This blending determines a trim attitude for a given rotorcraft flight condition.
申请公布号 US8694182(B2) 申请公布日期 2014.04.08
申请号 US20070695707 申请日期 2007.04.03
申请人 CHEREPINSKY IGOR;SIKORSKY AIRCRAFT CORPORATION 发明人 CHEREPINSKY IGOR
分类号 G05D1/00;G05D1/08;G05D3/00;G06F7/00;G06F17/00 主分类号 G05D1/00
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