发明名称 |
METHOD FOR MISSILE FLIGHT CONTROL |
摘要 |
FIELD: military equipment.SUBSTANCE: invention relates mainly to tactical and operational-tactical guided weapon systems (URO) with ballistic (aeroballistic) and high-altitude cruise missiles. Optical-electronic correlation-extremum CN missile additionally includes a laser altimeter (LV). Functioning of CN is started at a distance from target and missile flight altitude of 1…20 km, wherein when LV receives reflected signals of underlying surface above threshold level, method comprises correlation-extreme binding to underlying surface and correction of curved missile trajectory to end of flight. If LV receives reflected signals below threshold, method comprises performing a program manoeuvre of missile in plane of firing with output on section of flat glide at altitude of 100…500 m for 0.5…15.0 km from target, correlation-extreme binding to underlying surface and correction of glide trajectory of missile, with diving final section for 0.1…2.0 km from target, up to end of flight.EFFECT: invention widens weather range of application of missiles.1 cl, 2 dwg |
申请公布号 |
RU2595282(C1) |
申请公布日期 |
2016.08.27 |
申请号 |
RU20150128758 |
申请日期 |
2015.07.15 |
申请人 |
Aktsionernoe obshshestvo "Voenno-promyshlennaya korporatsiya "Nauchno-proizvodstvennoe obedinenie mashinostroeniya" |
发明人 |
Leonov Aleksandr Georgievich;Martynov Vyacheslav Ivanovich;Zimin Sergej Nikolaevich;Bolshakov Mikhail Valentinovich;Lavrenov Aleksandr Nikolaevich;Kulakov Aleksandr Valerevich;Petukhov Roman Andreevich;Ivanov Ilya Aleksandrovich;Svirin Nikolaj Stepanovich |
分类号 |
B64C19/00;F41G7/26;F42B15/01 |
主分类号 |
B64C19/00 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|