发明名称 CONTROL SYSTEM OF AIRCRAFT, METHOD FOR CONTROLLING AIRCRAFT, AND AIRCRAFT
摘要 <p>stable flight can be achieved without the need for a complicated throttle operation by a pilot even when part or all of control surfaces malfunction. A computation means (15) calculates a thrust control signal for controlling engine thrust and a deflection angle control signal for controlling control surfaces based on state information regarding an airframe, and an operation command signal from an operation end. An engine driving means (17) drives an engine based on the thrust control signal. A control surface moving means (16) moves the control surfaces based on the deflection angle control signal.</p>
申请公布号 EP2540621(A1) 申请公布日期 2013.01.02
申请号 EP20110747492 申请日期 2011.02.25
申请人 MITSUBISHI HEAVY INDUSTRIES, LTD. 发明人 YAMASAKI, KOICHI
分类号 B64C13/00 主分类号 B64C13/00
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