发明名称 |
System and method for gyro enhanced vertical flight information |
摘要 |
A flight instrument and associated method where vertical speed information is combined with gyro information to produce gyro enhanced vertical speed information that is displayed to a pilot. The gyro information may include a pitch rate gyro and may include an azimuth rate gyro. The pitch rate gyro and azimuth rate gyro may be combined to yield a corrected pitch rate in turns. In one embodiment, the display is an airplane symbol that moves relative to a horizon line responsive to the gyro enhanced vertical speed information. The horizon line may also tilt in response to the azimuth rate gyro.
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申请公布号 |
US7305286(B1) |
申请公布日期 |
2007.12.04 |
申请号 |
US20050263564 |
申请日期 |
2005.10.31 |
申请人 |
TRUTRAK FLIGHT SYSTEMS, INC. |
发明人 |
YOUNKIN JAMES R.;BILBE CHARLES R. |
分类号 |
G05D1/00;G01C19/00;G01C22/00;G05D1/08;G05D3/00;G06F7/00;G06F17/00;G06F19/00 |
主分类号 |
G05D1/00 |
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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