首页>
外国专利>
Flight path angle command, flight control system for landing flare
Flight path angle command, flight control system for landing flare
展开▼
机译:飞行路径角度指令,着陆弹道飞行控制系统
展开▼
页面导航
摘要
著录项
相似文献
摘要
0 This invention provides a flare control modification for pilot-in-the-loop aircraft maneuver command electronic flight control systems. During flare pilot pitch control inputs are interpreted as incremental flight path angle commands above a reference flight path angle (nominally a -3 glideslope). The flare control modification allows conventional piloting technique (i.e., pitch controller pull-and-hold) to be used during flare, while retaining the benefits of the maneuver command system masking effects of gusts, winds, windshear, and variations in airplane weight, balance, and aerodynamic configuration.
展开▼