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公开(公告)号:US09656593B2
公开(公告)日:2017-05-23
申请号:US14316053
申请日:2014-06-26
申请人: The Boeing Company
CPC分类号: B60Q1/08 , B60Q1/143 , B60Q2300/112 , B60Q2300/332 , G01C21/10 , G05D1/0808
摘要: An autopilot for a flight vehicle is described herein. Various configurations of the autopilot may be used in a gyro-less guidance and control system, which can be designed based on translational acceleration measurements only. In other configurations, the one or more components of the autopilot may be used as a backup to primary components of a guidance and control system. The autopilot may use state estimates to determine effector commands to control a flight vehicle.
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公开(公告)号:US20160231753A1
公开(公告)日:2016-08-11
申请号:US14316053
申请日:2014-06-26
申请人: The Boeing Company
CPC分类号: B60Q1/08 , B60Q1/143 , B60Q2300/112 , B60Q2300/332 , G01C21/10 , G05D1/0808
摘要: An autopilot for a flight vehicle is described herein. Various configurations of the autopilot may be used in a gyro-less guidance and control system, which can be designed based on translational acceleration measurements only. In other configurations, the one or more components of the autopilot may be used as a backup to primary components of a guidance and control system. The autopilot may use state estimates to determine effector commands to control a flight vehicle.
摘要翻译: 这里描述了用于飞行器的自动驾驶仪。 自动驾驶仪的各种配置可用于无陀螺仪的引导和控制系统,该系统只能基于平移加速度测量设计。 在其他配置中,自动驾驶仪的一个或多个部件可以用作对引导和控制系统的主要部件的备份。 自动驾驶仪可以使用状态估计来确定效应器命令来控制飞行器。
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