发明名称 METHOD OF CONTROL OF ANGULAR MOTION OF AIRCRAFT WITH INTEGRATING DRIVE
摘要 FIELD: physics. ^ SUBSTANCE: invention is related to the field of instrument making and may be used for control of angular motion of aircrafts. Method provides formation of optimal indices of transition processes by coordinates of angular motion of aircraft. At that control of aircraft is carried out without correction of proportionality coefficients of control laws of angular motion of aircraft in full operation range of changes of velocities and altitudes of flight, and also for channel of pitch and during change of aircraft alignment in the process of motion. ^ EFFECT: expansion of functional resources of device for control of angular motion of aircrafts. ^ 6 dwg
申请公布号 RU2335005(C1) 申请公布日期 2008.09.27
申请号 RU20070104892 申请日期 2007.02.08
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 G05D1/00 主分类号 G05D1/00
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