专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明申请

WO2017209796A1 SOFTWARE CONTROLLED STIFFENING OF FLEXIBLE AIRCRAFT 审中-公开
标题翻译：柔性飞机的软件控制加强
公开(公告)号：WO2017209796A1
公开(公告)日：2017-12-07
申请号：PCT/US2016/069608
申请日：2016-12-30
申请人： GOOGLE LLC
发明人： KREBS, Mark , BRANDMEYER, Jonathan Daniel
IPC分类号： B64C3/52 , B64C13/16 , B64C39/10 , G05D1/08
CPC分类号： B64C13/18 , B64C3/38 , B64C3/52 , B64C9/04 , B64C13/16 , B64C39/10 , B64C2201/021 , B64C2201/028 , B64C2201/104 , G05D1/0841
摘要： Systems and methods for operating control surfaces of an aircraft. The method involves receiving, by an aircraft control system from one or more sensors, deflection information related to a shape and motion of an aircraft, and decomposing, by the aircraft control system, the deflection information into a detected modal state including a first known mode having a first mode strength. The method may further involve determining, by the aircraft control system, a first modal compensation based on the first mode strength, and identifying, by the aircraft control system, a desired control corresponding to a second known mode. The method may yet further involve determining a first control response for a control surface having a first modal weight and a second modal weight, based on the first modal compensation and the first modal weight, and determining a second control response for the control surface based on the desired control and the second modal weight. The method may still further involve generating a control command for the control surface based on the first control response and the second control response.
摘要翻译：
用于操作飞机的控制表面的系统和方法。该方法包括由飞行器控制系统从一个或多个传感器接收与飞行器的形状和运动有关的偏转信息，并且由飞行器控制系统将偏转信息分解为包括第一已知模式的检测模态具有第一模式强度。该方法还可以包括由飞行器控制系统基于第一模式强度确定第一模态补偿并且由飞行器控制系统识别与第二已知模式相对应的期望控制。该方法还可以包括基于第一模态补偿和第一模态权重确定具有第一模态权重和第二模态权重的控制表面的第一控制响应，并且基于第一模态补偿和第一模态权重确定用于控制表面的第二控制响应期望的控制和第二模态重量。该方法还可以涉及基于第一控制响应和第二控制响应来产生用于控制表面的控制命令。

IPRDB

热门服务

关于我们

友情链接

联系方式