发明名称 |
Arithmetic processing method and system in a wide velocity range flight velocity vector measurement system using a square truncated pyramid-shape five-hole pitot probe |
摘要 |
An arithmetic processing method and system in a wide velocity range flight velocity vector measurement system using a square truncated pyramid-shape five-hole Pitot probe. Approximation equations that determine attack angle alpha and sideslip angle beta in the form of third-order equations concerning attack angle pressure coefficient Calpha and sideslip angle pressure coefficient Cbeta, which are known numbers, are expressed in the form of a polynomial equation concerning Mach number M, where the coefficients are obtained from a lookup table. Coefficient calculations in the polynomial equation, and attack angle a and sideslip angle beta, calculations may be performed as simple calculations by specifying and applying known numbers into the approximation equation without solving third-order equations, with calibration coefficients that form the basis of coefficient calculation with the polynomial equation first being stored in memory in advance as a table for each wide velocity range on the basis of wind tunnel testing. A Mach number may be calculated instantly from a lookup table by specifying Mach pressure coefficient CM and angle to airflow pressure coefficient Cgamma. Wide velocity range flight velocity vector measurement with a high update rate which is capable of real time response in flight control as demanded by aircraft is obtained.
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申请公布号 |
US6336060(B1) |
申请公布日期 |
2002.01.01 |
申请号 |
US20000661411 |
申请日期 |
2000.09.13 |
申请人 |
NATIONAL AEROSPACE LABORATORY OF SCIENCE AND TECHNOLOGY AGENCY |
发明人 |
SHIGEMI MASASHI;NAKAYA TERUOMI;SHINDO SHIGEMI;TAKIZAWA MINORU;OHNUKI TAKESHI |
分类号 |
G01P5/175;G01L7/00;G01P5/16;G01P5/165;G01P13/02;(IPC1-7):G01C21/10 |
主分类号 |
G01P5/175 |
代理机构 |
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地址 |
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