| 发明名称 |
LOW SPEED MODEL FOLLOWING VELOCITY COMMAND SYSTEM FOR ROTARYWING AIRCRAFT |
| 摘要 |
<p>A rate model algorithm responsive to the pilot attitude command signal, flight parameters sensors and an inverse vehicle model algorithm provide signals to rotary wing aircraft flight command to get the aerodynamical response to the pilot command.</p> |
| 申请公布号 |
CA2116565(C) |
申请公布日期 |
2000.07.04 |
| 申请号 |
CA19922116565 |
申请日期 |
1992.08.21 |
| 申请人 |
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发明人 |
GOLD, PHILLIP J.;GLUSMAN, STEVEN I.;FOGLER, DONALD L., JR.;RICHARD, JAMES L. |
| 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 |
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代理人 |
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