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 |
AU655845(B2) |
申请公布日期 |
1995.01.12 |
申请号 |
AU19920025981 |
申请日期 |
1992.08.21 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
DONALD L. FOGLER JR.;JAMES L RICHARD;PHILLIP J GOLD;STEVEN I GLUSMAN |
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;(IPC1-7):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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