| 发明名称 |
FLIGHT GUIDANCE AND CONTROL COMPLEX FOR FLYING VEHICLES |
| 摘要 |
FIELD: aeronautical engineering. SUBSTANCE: flight guidance and control complex includes control unit, programmed motion parameter forming unit, motion parameter sensor unit, disturbing action sensor unit, two interpolation polynomial shaping units which are built on delay units, coefficient shaping unit and summing amplifier. Complex ensures optimization of initial conditions at preset quality of control and accurate performance of flight over time-and-spatial trajectory at disturbing action. EFFECT: enhanced accuracy of flight. 2 cl, 2 dwgf
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| 申请公布号 |
RU2112268(C1) |
申请公布日期 |
1998.05.27 |
| 申请号 |
RU19960124269 |
申请日期 |
1996.12.25 |
| 申请人 |
AKTSIONERNOE OBSHCHESTVO OTKRYTOGO TIPA "MOSKOVSKI;AKTSIONERNOE OBSHCHESTVO OTKRY |
发明人 |
VAJNBERG M.V.;DZHANDZHGAVA G.I.;ZHOSAN N.V.;NEGRIKOV V.V.;POLOSENKO V.P.;PTITSYN A.N.;SHELEPEN' K.V.;SHCHERBINA V.G.;VAJNBERG M.V.;DZHANDZHGAVA G.I.;ZHOSAN N.V.;NEGRIKOV V.V.;POLOSENKO V.P.;PTITSYN A.N.;SHELEPEN' K.V.;SHCHERBINA V.G. |
| 分类号 |
G05B13/04;B64C13/18;(IPC1-7):G05B13/04 |
主分类号 |
G05B13/04 |
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