发明名称 |
AUTOPILOT FOR SYMMETRICAL GUIDED ANTI-AIRCRAFT MISSILE |
摘要 |
FIELD: guidance of missiles; autopilots for guided anti-aircraft missiles of symmetrical aerodynamic configuration. ^ SUBSTANCE: autopilot includes two identical lateral control channels; each lateral control channel includes lateral acceleration error signal shaper and shaper of signal for control of drive of pair of control surfaces lying in one plane which are connected in series; autopilot has also bank angle control channel including bank angle error signal shaper and shaper of signal for control of all control surfaces of missile which are connected in series. Besides that, auto-pilot is provided with compensation unit for compensating for aerodynamic interaction of channels; output of compensation unit is connected to second input of adder whose first input is connected to output of bank angle control channel. ^ EFFECT: enhanced accuracy of control of guided anti-aircraft missiles. ^ 2 cl, 3 dwg |
申请公布号 |
RU2302358(C1) |
申请公布日期 |
2007.07.10 |
申请号 |
RU20060102575 |
申请日期 |
2006.01.31 |
申请人 |
OTKRYTOE AKTSIONERNOE OBSHCHESTVO "NAUCHNO-PROIZVODSTVENNOE OB"EDINENIE "ALMAZ" IMENI AKADEMIKA A.A. RASPLETINA";OTKRYTOE AKTSIONERNOE OBSHCHESTVO "MASHINOSTROITEL'NOE KONSTRUKTORSKOE BJURO "FAKEL" IMENI AKADEMIKA P.D. GRUSHINA" |
发明人 |
BUDILIN VSEVOLOD ALEKSANDROVICH;MIZROKHI VLADIMIR JAKOVLEVICH;PUTSYKOVICH DMITRIJ VJACHESLAVOVICH |
分类号 |
B64C13/18;G05D1/00 |
主分类号 |
B64C13/18 |
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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