RU2013149443A - METHOD OF MANAGEMENT OF FLIGHT MISSILES AT FLIGHT TEST - Google Patents
METHOD OF MANAGEMENT OF FLIGHT MISSILES AT FLIGHT TEST Download PDFInfo
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- RU2013149443A RU2013149443A RU2013149443/11A RU2013149443A RU2013149443A RU 2013149443 A RU2013149443 A RU 2013149443A RU 2013149443/11 A RU2013149443/11 A RU 2013149443/11A RU 2013149443 A RU2013149443 A RU 2013149443A RU 2013149443 A RU2013149443 A RU 2013149443A
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- rocket
- flight
- liquidation
- missile
- places
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- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Способ управления полетом ракеты при летных испытаниях, включающий определение текущих координат и параметров движения ракеты, расчет вероятной траектории, формирование и передачу на ракету команд на изменение траектории полета, а также постоянную передачу на командный пункт данных о состоянии окружающей среды на трассе летных испытаний, прогноз возможного нештатного изменения траектории полета, приводящее к загрязнению поверхности земли, водоемов и воздуха, передачу на ракету команд либо на продолжение полета к цели, либо на отклонение от траектории и уничтожение ракеты в районе с минимальным ущербом для окружающей среды, отличающийся тем, что с помощью бортового радиолокационного комплекса дистанционного зондирования Земли штатное и прогнозируемое места уничтожения ракеты в результате возможного нештатного изменения траектории полета, постоянно обследуют в течении всего отрезка времени от установки ракеты в пусковую установку до ее пуска, регистрируют в обоих местах появление несанкционированных объектов, существование которых подвергается опасности при самоликвидации ракеты, фиксируют их, выявляют и идентифицируют несанкционированные объекты, одновременно вводят в программную систему управления полетом команду отсрочки момента самоликвидации и далее, если к моменту пуска ракеты несанкционированные объекты все еще будут находится в одном из мест ликвидации ракеты, включают команду отсрочки самоликвидации ракеты или отвода ее в безопасное место.A method of controlling a missile’s flight during flight tests, including determining the current coordinates and parameters of the rocket’s movement, calculating the probable trajectory, generating and transmitting commands to the missile to change the flight path, as well as constantly transmitting environmental data to the command post along the flight test route, forecast possible abnormal changes in the flight path, leading to contamination of the surface of the earth, water bodies and air, transmission of commands to the rocket either to continue the flight to the target, or to deviate from the trajectory and the destruction of a rocket in an area with minimal environmental damage, characterized in that with the help of an onboard radar system for remote sensing of the Earth, the regular and predicted places of destruction of a rocket as a result of a possible abnormal change in the flight path are constantly examined over the entire period of time from installation missiles in the launcher prior to its launch, register in both places the appearance of unauthorized objects, the existence of which is endangered when the missile’s elimination, fix them, identify and identify unauthorized objects, at the same time enter the command to delay the moment of self-liquidation into the flight control software system, and if, by the time the rocket is launched, unauthorized objects will still be in one of the places of the rocket liquidation, include the command to delay the self-liquidation of the rocket or taking her to a safe place.
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Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2013149443/11A RU2549425C1 (en) | 2013-11-06 | 2013-11-06 | Method of controlling rocket flight during flight tests |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2013149443/11A RU2549425C1 (en) | 2013-11-06 | 2013-11-06 | Method of controlling rocket flight during flight tests |
Publications (2)
Publication Number | Publication Date |
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RU2549425C1 RU2549425C1 (en) | 2015-04-27 |
RU2013149443A true RU2013149443A (en) | 2015-05-20 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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RU2013149443/11A RU2549425C1 (en) | 2013-11-06 | 2013-11-06 | Method of controlling rocket flight during flight tests |
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RU (1) | RU2549425C1 (en) |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2114374C1 (en) * | 1994-09-30 | 1998-06-27 | Товарищество с ограниченной ответственностью ВНПП "Эрток" | Method of missile flight control in flight tests |
US20090105892A1 (en) * | 2007-10-19 | 2009-04-23 | Draughon Ryan J | Telemetry analysis system networked data acquisition system |
RU88168U1 (en) * | 2009-05-20 | 2009-10-27 | Ольга Петровна Куркова | SYSTEM OF CENTRALIZED AUTOMATED FUNCTIONAL AND ECONOMIC MANAGEMENT IN REAL TIME BY THE CONSORTIUM FOR CREATION OF SPACE SYSTEMS FOR REMOTE SENSING OF THE EARTH SURFACE |
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2013
- 2013-11-06 RU RU2013149443/11A patent/RU2549425C1/en active
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Publication number | Publication date |
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RU2549425C1 (en) | 2015-04-27 |
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