| 发明名称 |
Low Speed Model Following Velocity Command System for Rotary Wing Aircraft |
| 摘要 |
<p>A helicopter flight control system (21) includes a model following control system architecture which operates in a velocity command mode at low ground speeds. The control system processes information from a variety of helicopter sensors (31) in order to provide a command signal to the main rotor (11) of the helicopter which results in a ground speed which is proportional to the input provided via a sidearm controller (29).</p> |
| 申请公布号 |
CA2116565(A1) |
申请公布日期 |
1993.03.18 |
| 申请号 |
CA19922116565 |
申请日期 |
1992.08.21 |
| 申请人 |
UNITED TECHNOLOGIES CORP |
发明人 |
FOGLER DONALD L JR;RICHARD JAMES L;GOLD PHILLIP J;GLUSMAN STEVEN I |
| 分类号 |
A61K31/40;A61K31/4025;A61K31/435;A61P1/00;A61P9/00;A61P9/10;A61P9/12;A61P11/00;A61P11/08;A61P13/02;A61P15/00;B64C13/18;B64C27/12;C07D405/04;G05D1/00;G05D1/06;G05D1/08 |
主分类号 |
A61K31/40 |
| 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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