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 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|