发明名称 |
Method of inferring rotorcraft gross weight |
摘要 |
Described are systems and methods for determining the gross weight of an aircraft. A flight regime is determined based on one or more inputs. A neural net is selected based on a flight regime. The neural net inputs may include derived values. A first estimate of the gross weight is produced by the selected neural net. The first estimate is used, along with other inputs, with a Kalman filter to produce a final gross weight estimate. The Kalman filter blends or fuses together its inputs to produce the final gross weight estimate.
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申请公布号 |
US2004193386(A1) |
申请公布日期 |
2004.09.30 |
申请号 |
US20040779365 |
申请日期 |
2004.02.13 |
申请人 |
FLYNN TIMOTHY D.;HESS ROBERT ALAN;NOBLE BARBARA |
发明人 |
FLYNN TIMOTHY D.;HESS ROBERT ALAN;NOBLE BARBARA |
分类号 |
G01G19/07;G06F17/17;(IPC1-7):G06E1/00;G06E3/00;G06G7/00;G06F15/18;G01G7/00;G01G9/00;G01G11/00;G06F15/00;G06F15/02;G01G17/00;G01G19/00 |
主分类号 |
G01G19/07 |
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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