发明名称 CONTROL DEVICE OF FLYING MACHINE
摘要 PROBLEM TO BE SOLVED: To provide a technique early exhibiting output in an emergency. SOLUTION: In the control device of a flying machine, when two units of engines are in normal state, the thrust of an air frame and an attitude control are performed by a uniform output of both engines, and when one of two engines fails to operate properly, the thrust of the air frame and the attitude are controlled by increasing the output of the other normal engine up to the output in the emergency. When one engine fails to operate properly, the output of the engine used for the thrust of the air frame and the attitude control is reduced lower than the output of engine used when two engines are in normal state until the other normal engine can output the output in the emergency. COPYRIGHT: (C)2007,JPO&INPIT
申请公布号 JP2007022268(A) 申请公布日期 2007.02.01
申请号 JP20050206002 申请日期 2005.07.14
申请人 TOYOTA MOTOR CORP 发明人 FUKUDA HIROYOSHI
分类号 B64D31/04;B64C29/04 主分类号 B64D31/04
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