GR990100359A - A guidance system for a short-range anti-aircraft missile unit - Google Patents
A guidance system for a short-range anti-aircraft missile unitInfo
- Publication number
- GR990100359A GR990100359A GR990100359A GR990100359A GR990100359A GR 990100359 A GR990100359 A GR 990100359A GR 990100359 A GR990100359 A GR 990100359A GR 990100359 A GR990100359 A GR 990100359A GR 990100359 A GR990100359 A GR 990100359A
- Authority
- GR
- Greece
- Prior art keywords
- missile
- tracking
- radar
- evaluator
- range
- Prior art date
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/66—Radar-tracking systems; Analogous systems
- G01S13/72—Radar-tracking systems; Analogous systems for two-dimensional tracking, e.g. combination of angle and range tracking, track-while-scan radar
- G01S13/723—Radar-tracking systems; Analogous systems for two-dimensional tracking, e.g. combination of angle and range tracking, track-while-scan radar by using numerical data
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
- F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
- F41G7/30—Command link guidance systems
- F41G7/301—Details
- F41G7/303—Sighting or tracking devices especially provided for simultaneous observation of the target and of the missile
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Radar Systems Or Details Thereof (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
Abstract
The invention relates to radar engineering and is suitable to be used in the aerial defence guided weapon systems. The guidance system comprises, mounted on a single self-propelled carrier or in a conveyance container, a detection means having an all round looking radar, a radar-based identification interrogator, means for tracking and precision-measurement of the target and missile coordinates, an information display means, devices for the missile pre-launch preparation and launch execution, computation control means, comprising an evaluator for evaluating the time a target enters the launch area and an angle misalignment evaluator; a range and launch area and an angle misalignment evaluator; a range and azimuth tracking device, a system for controlling the tracking radar beam whose antenna isimplemented in the form of a phased array, a programmable search device, a system for simultaneous tracking basing on four coordinates (azimuth, elevation, range and Doopler frequency) of a number of objects using a tracking radar of a missile beacon, a switching device, a tracking radar of the missile transponder, a missile beacon, a tracking radar of a missile beacon, a switching device, a device for identifying the target class and adapting the modes of operation of the missile control systems, including a signal spectral analysis unit, an evaluator for evaluating the prelaunch command information and missile deviation angles after the vertical launch. This system allows to improve the combat efficiency of short-range missile systems in defence against small-size and high-speed targets of the new class owing to a decreased time of response of their control systems
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EA199900050A EA002202B1 (en) | 1998-10-19 | 1998-10-19 | A guidance system for a short-range anti-aircraft missile unit |
Publications (2)
Publication Number | Publication Date |
---|---|
GR990100359A true GR990100359A (en) | 2000-06-30 |
GR1003436B GR1003436B (en) | 2000-09-19 |
Family
ID=8161478
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GR990100359A GR1003436B (en) | 1998-10-19 | 1999-10-18 | A guidance system for a short-range anti-aircraft missile unit |
Country Status (4)
Country | Link |
---|---|
CA (1) | CA2325146A1 (en) |
EA (1) | EA002202B1 (en) |
GR (1) | GR1003436B (en) |
WO (1) | WO2000023819A1 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2461843C1 (en) * | 2011-04-29 | 2012-09-20 | Открытое акционерное общество "Федеральный научно-производственный центр "Нижегородский научно-исследовательский институт радиотехники" | Method of processing radar information in network information structure of automated control system |
CN109583132B (en) * | 2018-12-18 | 2023-04-07 | 中国人民解放军国防科技大学 | Hypersonic aircraft landing probability calculation method based on radar detection error |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0260191A1 (en) * | 1986-09-09 | 1988-03-16 | Thomson-Csf | Process and device for displaying targets or target positions using the data acquisition means of a weapon system |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1601829A (en) * | 1978-05-08 | 1981-11-04 | Raytheon Co | Vehicle guidance apparatus |
EP0276530B1 (en) * | 1987-01-28 | 1992-11-11 | Hercules Incorporated | Millimeter wave length guidance system |
US4665401A (en) * | 1980-10-10 | 1987-05-12 | Sperry Corporation | Millimeter wave length guidance system |
DE3318340C1 (en) * | 1983-05-20 | 1992-03-05 | Siemens Ag | Procedure for tracking target objects |
NL1004025C2 (en) * | 1996-09-13 | 1998-03-16 | Hollandse Signaalapparaten Bv | Method for determining an impact point of a fired projectile with respect to a target. |
-
1998
- 1998-10-19 EA EA199900050A patent/EA002202B1/en not_active IP Right Cessation
-
1999
- 1999-09-28 WO PCT/EA1999/000007 patent/WO2000023819A1/en active Application Filing
- 1999-09-28 CA CA002325146A patent/CA2325146A1/en not_active Abandoned
- 1999-10-18 GR GR990100359A patent/GR1003436B/en not_active IP Right Cessation
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0260191A1 (en) * | 1986-09-09 | 1988-03-16 | Thomson-Csf | Process and device for displaying targets or target positions using the data acquisition means of a weapon system |
Also Published As
Publication number | Publication date |
---|---|
EA002202B1 (en) | 2002-02-28 |
EA199900050A1 (en) | 2000-04-24 |
CA2325146A1 (en) | 2000-04-27 |
GR1003436B (en) | 2000-09-19 |
WO2000023819A1 (en) | 2000-04-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ML | Lapse due to non-payment of fees |