发明名称 |
HIGHLY-MANEUVERABLE AIRCRAFT CROSS-RANGE MANEUVERING AUTOMATIC CONTROL SYSTEM |
摘要 |
FIELD: aircraft engineering. ^ SUBSTANCE: control stick displacement is used as a parametre related with pilot actions. Control signals are generated in bank and yaw channels to vary as control stick displacement. Damping isodromic signals of bank and yaw angular speeds are generated with their magnitudes, if minor, are taken to equal zero. Generated signals are summed up to be dynamically constricted by integrating links of appropriate bank and yaw channel pre-filters. Said signals are used as feedback signals sent to integrating link inputs when their absolute values exceed constriction values. Said signals are additionally summed with appropriate damping isodromic signals of bank and yaw angular speeds, earlier taken to equal zero. Shaped control signals are fed to inputs of appropriate drives to displace ailerons and rudder. ^ EFFECT: optimum aircraft control. ^ 1 dwg |
申请公布号 |
RU2383467(C1) |
申请公布日期 |
2010.03.10 |
申请号 |
RU20080139961 |
申请日期 |
2008.10.09 |
申请人 |
OTKRYTOE AKTSIONERNOE OBSHCHESTVO MOSKOVSKIJ NAUCHNO-PROIZVODSTVENNYJ KOMPLEKS "AVIONIKA" (OAO MNPK"AVIONIKA") |
发明人 |
VOROB'EV ALEKSANDR VLADIMIROVICH;SHTEJNGARDT BORIS KHASKEL'EVICH;MOZHAROV VALERIJ ALEKSEEVICH |
分类号 |
B64C13/18 |
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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