发明名称 DEVICE FOR DETERMINATION OF AEROSPACE TARGET MOTION PARAMETRES IN ACTUAL TIME SCALE
摘要 FIELD: physics, measurements. ^ SUBSTANCE: invention is related to the field of determination of spatial parametres of flying target motion, for instance in case of training aviation or rocket-space attack, and may be used in development of facilities for detection, registration, seizure and surveillance over flying aerospace targets with nonrecurrent processing of measurement results in actual time scale and automatic tracking of measurement objects from mobile and/or stationary metering posts for provision of possibility for destruction of objects. Device for determination of trajectory flight parametres of target motion in actual time scale includes complex of target flight parametres registration, comprising unit of photo-optical registration of trajectory parametres of target and unit for fixation of dynamic parametres of target by trajectory of observance, which functionally interact with unit of control and digital processing of measurement results, besides, complex of flight parametres registration is installed on rotary-support reference base with the possibility of azimuth-horizontal arc inertia-free motion relative to fixed axis of base reference point during target scanning, besides system of target flight parametres registration is additionally equipped with device of scanning and registration of fighting gear burst, which is functionally connected to unit of photo-optical registration of flight parametres with creation of module of automatic scanning, detection, registration and target tracking system, which is installed with the possibility of continuous-discrete scanning of trajectory parametres of the latter during azimuth-horizontal displacement of created unit of automatic scanning system. ^ EFFECT: improved stability of determination of non-identified targets motion parametres by provision of possibility of detection, automatic seizure and further continuous tracking of dynamic objects of aviation and rocket-space engineering in different flight modes with provision of possibility to determine parametres of mutual location of flying objects in continuous mode during registration of their flight trajectory and time of fighting gear actuation at the moment of explosion for a day under complicated meteorological conditions, in stabilisation of continuous mode of object tracking system control process, with optimisation of parametres of annular divergence with increase of target detection and registration distance range. ^ 3 cl
申请公布号 RU2366975(C1) 申请公布日期 2009.09.10
申请号 RU20070147373 申请日期 2007.12.21
申请人 FEDERAL'NOE GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "KONSTRUKTORSKOE BJURO TRANSPORTNOGO MASHINOSTROENIJA" (FGUP KBTM) 发明人 GONCHAR ALEKSANDR ALEKSEEVICH;GONCHAR ALEKSEJ GRIGOR'EVICH;KOLJUBIN ANATOLIJ VASIL'EVICH;RYSEV VLADIMIR VLADIMIROVICH;SHAPOVALOV RUSLAN VASIL'EVICH
分类号 G01S17/06 主分类号 G01S17/06
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