发明名称 SIGHTING NAVIGATIONAL COMPLEX FOR MULTI-MISSION AIRCRAFT
摘要 FIELD: aeronautical engineering; onboard electronic equipment used for navigation and guidance; use of counter-measures. ^ SUBSTANCE: proposed complex includes set of multi-functional indicators interconnected by inputs and outputs in information exchange channel, windshield indicator, outside-cabin observation TV camera, on-line control elements, set of observation and sighting means, set of navigational and pilotage means, portable initial data carrier, counter-measure control system and computer system. Computer system includes logic elements of combined data base interconnected by inputs and outputs in computer information exchange line, elements of forming navigational and pilotage parameters, sighting and pilotage parameters, forming displayed information, input, output and control of information exchange, synthesizing parameters of motion relative to air medium, synthesizing target designation parameters, control of combat situation and training situations. ^ EFFECT: extended functional capabilities; enhanced efficiency of multi-mission aircraft. ^ 1 dwg
申请公布号 RU2263881(C1) 申请公布日期 2005.11.10
申请号 RU20040138493 申请日期 2004.12.29
申请人 发明人 GUSHCHIN G.M.;DZHANDZHGAVA G.I.;KAVINSKIJ V.V.;KOZOROVETSKIJ A.N.;KOZYREV V.P.;LOBKO S.V.;NEGRIKOV V.V.;OREKHOV M.I.;SEMASH A.A.;SHKRED V.K.
分类号 G01C23/00;B64C15/00;B64D7/00 主分类号 G01C23/00
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