发明名称 Flight control system
摘要 <p>A backup engines-only flight control system accomplishes improved aircraft banking in response to commands by the use of a lead compensated transient differential thrust servo parameter (65). The lead compensated transient differential thrust servo parameter (65) compensates for the ordinary sluggish banking response during engines-only flight control. Accordingly, because an aircraft equipped with the present invention will respond in a manner expected by pilots, safer backup engines-only flight control is achieved during emergency situations. The improvement comprises a means and method of detecting the magnitude of direction of commanded bank angle and generating a corresponding lead compensated transient differential thrust servo parameter (65). &lt;IMAGE&gt;</p>
申请公布号 EP1011036(A1) 申请公布日期 2000.06.21
申请号 EP19990124445 申请日期 1999.12.08
申请人 HONEYWELL INC. 发明人 KAHLER, JEFFREY
分类号 G05D1/04;G05D1/06;(IPC1-7):G05D1/02 主分类号 G05D1/04
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