发明名称 |
Coriolis indicator for situational awareness |
摘要 |
A system for indicating the presence of Coriolis accelerations within an aircraft which might affect pilot perception of aircraft attitude and spatial orientation, which comprises sensors for measuring vehicle angular position, rotations and velocities operatively connected to an onboard computer program which calculates the Coriolis accelerations according to an analysis presented herein and presented on a display to the pilot.
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申请公布号 |
US5353226(A) |
申请公布日期 |
1994.10.04 |
申请号 |
US19920934226 |
申请日期 |
1992.08.25 |
申请人 |
THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE AIR FORCE |
发明人 |
REPPERGER, DANIEL W. |
分类号 |
G01P9/00;G01P9/04;G01P15/18;(IPC1-7):G01P9/04 |
主分类号 |
G01P9/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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