发明名称 Aircraft throttle control system - has shear detector and compensator to reduce speed variation during moderate and heavy turbulence and incorporates gust bias provision
摘要 <p>The system is for processing signals representative of airspeed error and inertial longitudinal acceleration in two channels, respectively, and providing cancellation of the turbulence-induced components of the respective signals. Shear detection and compensation circuits are provided in the system for reducing speed wandering in moderate and heavy turbulence. A circuit processing the signal from the shear detector circuit is utilised to provide a gust bias signal input in the system.</p>
申请公布号 IT1115011(B) 申请公布日期 1986.02.03
申请号 IT19790048064 申请日期 1979.02.21
申请人 THE BOEING CO 发明人
分类号 B64D;(IPC1-7):B64D/ 主分类号 B64D
代理机构 代理人
主权项
地址