发明名称 BAROMETRIC ALTIMETER FOR FLYING BODY AND ITS ERROR CORRECTION METHOD
摘要 PROBLEM TO BE SOLVED: To provide a barometric altimeter and its error correction method capable of correctly detecting the altitude of a flying body only using the barometric measurement without using information regarding the body attitude or speed, and without deceleration by using a deceleration device. SOLUTION: The flying body comprises: a barometric altimeter 10 for detecting the altitude of the flying body 1 having a cylindrical outer surface 2a with a center axis in a flying direction x; a plurality of static pressure holes 12 provided in a constant interval from the top of flying direction on the cylindrical outer surface 2a; a mean static pressure detector 14 for detecting the mean static pressure of the plurality of the static pressure holes; a total pressure detector 16 provided on the top of the flying direction for detecting the total pressure; and an altitude operation device 18 for calculating the altitude by correcting the mean static pressure during flying with the detected mean static pressure and the total pressure. COPYRIGHT: (C)2005,JPO&NCIPI
申请公布号 JP2005147726(A) 申请公布日期 2005.06.09
申请号 JP20030381932 申请日期 2003.11.12
申请人 IHI AEROSPACE CO LTD 发明人 KANEDA MORIAKI;TOGANO HAKUSHI
分类号 F42B15/01;G01C5/06;(IPC1-7):G01C5/06 主分类号 F42B15/01
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