| 发明名称 |
METHOD OF LONGITUDINAL CONTROL OF AIRPLANE |
| 摘要 |
FIELD: physics, aviation. ^ SUBSTANCE: additional correcting signal is generated requiring no correction of factors of airplane control laws proportionality in all operating ranges of the flight altitude and speed changes. Note here that there is no necessity in controlling the flying aircraft centering variations. ^ EFFECT: expanded performances. ^ 4 dwg |
| 申请公布号 |
RU2344460(C1) |
申请公布日期 |
2009.01.20 |
| 申请号 |
RU20070112577 |
申请日期 |
2007.04.04 |
| 申请人 |
KAZANSKIJ GOSUDARSTVENNYJ TEKHNICHESKIJ UNIVERSITET IM. A.N. TUPOLEVA |
发明人 |
ROMANENKO LEONID GEORGIEVICH;ZAJTSEV SERGEJ VALENTINOVICH;SAMAROVA GUL'NAZ GARIFJANOVNA |
| 分类号 |
G05D1/08 |
主分类号 |
G05D1/08 |
| 代理机构 |
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