发明名称 ADAPTIVE SYSTEM FOR CONTROLLING FLIGHT HEIGHT OF AN AIRCRAFT
摘要 FIELD: engineering of onboard systems for automatic control of aircrafts, which during flight realize turns at significant angles of attack. ^ SUBSTANCE: control system contains aircraft as control object, steering drive, device for measuring angular position by pitch, adding amplifier, speed force indicator, indicator of height and height alternation speed, flight speed indicator, height signal set-point device, discrepancy block, first signal limiting block, functional transformer, second signal limiting block, functional device for limiting signal, first set-point device of bearing signal, first division block and first multiplication block, while functional transformer contains two of each of the following: set-point device of bearing signal, division block, multiplication block and adder. ^ EFFECT: expanded functional capabilities, limitation of angle of attack of an aircraft. ^ 2 cl, 3 dwg
申请公布号 RU2279119(C1) 申请公布日期 2006.06.27
申请号 RU20050102643 申请日期 2005.02.04
申请人 发明人 SYROV ANATOLIJ SERGEEVICH;TRUSOV VLADIMIR NIKOLAEVICH;LARIONOV VITALIJ ALEKSANDROVICH;ABADEEV EHDUARD MATVEEVICH;DUBINKIN IGOR' MIKHAJLOVICH;KRAVCHUK SERGEJ VALENTINOVICH;MAKAROV NIKOLAJ VALENTINOVICH;PUCHKOV ALEKSANDR MIKHAJLOVICH
分类号 G05D1/04 主分类号 G05D1/04
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