发明名称 ENGINE FUEL CONTROL DEVICE
摘要 PROBLEM TO BE SOLVED: To fly a flying body with prescribed thrust by automatically controlling fuel supplied to an engine to propel the flying body, to a flow quantity for generating thrust to attain the flying speed and altitude required of the flying body. SOLUTION: This engine fuel control device is provided with an accelerometer 4 for detecting the acceleration of the flying body; a gyroscope 5 for detecting angular velocity; an altimeter 6 for detecting altitude; a launching apparatus 3 for detecting launching initial speed; and a control part 21 inputting the acceleration, angular speed and launching initial speed to compute flying speed, comparing it with specified speed in each position of a prescribed trajectory, computing a fuel flow command to obtain fuel flow to make the flying speed coincide with the specified speed to output it to a fuel valve, and correcting to a fuel flow command for increasing the flying speed to heighten the flying altitude when the flying altitude is less than the predetermined altitude, and outputting it to the fuel valve. COPYRIGHT: (C)2004,JPO
申请公布号 JP2004060480(A) 申请公布日期 2004.02.26
申请号 JP20020217489 申请日期 2002.07.26
申请人 TECH RES & DEV INST OF JAPAN DEF AGENCY 发明人 YANO HIROSHI
分类号 F42B10/38;B64C13/18;F02C9/28;F02K1/15;F42B10/66;F42B15/01;(IPC1-7):F02K1/15 主分类号 F42B10/38
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