GB1535338A - Radar systems - Google Patents
Radar systemsInfo
- Publication number
- GB1535338A GB1535338A GB4682975A GB4682975A GB1535338A GB 1535338 A GB1535338 A GB 1535338A GB 4682975 A GB4682975 A GB 4682975A GB 4682975 A GB4682975 A GB 4682975A GB 1535338 A GB1535338 A GB 1535338A
- Authority
- GB
- United Kingdom
- Prior art keywords
- switch
- value
- target
- radar
- nov
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 230000001133 acceleration Effects 0.000 abstract 3
- 230000007704 transition Effects 0.000 abstract 1
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
- G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
- G01S7/02—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
- G01S7/28—Details of pulse systems
- G01S7/285—Receivers
- G01S7/292—Extracting wanted echo-signals
Landscapes
- Engineering & Computer Science (AREA)
- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
1535338 Radar SIEMENS AG 13 Nov 1975 [13 Nov 1974] 46829/75 Heading H4D A radar system is provided with means for detecting manoeuvres of the target in the form of changes in the state of motion, in particular any transition from zero acceleration using a radar receiver incorporating two Kalman filters for the optimum estimation of a variable parameter, the first, for analysing low level target accelerations and the second for higher order accelerations. In Fig. 9, echo signals U are fed to radar receiver Ra where they are converted to digital signals Z k and applied to computer Re. Switch S, controlled by threshold detector Sw is set to connect signals Sk to a 1st low-level Kalman filter Fl, when no manoeuvre is detected. Filter Fl produces estimated values of a state vector #X k representative of the target's position from which a prediction value #X k - is derived. The innovation value I k is formed by the correlation means to establish the difference between each measured value and the relevant prediction value and fed to a shift register Sr of length N. To complete the correlation the numerical values stored in the shift registered positions are then multiplied by respective estimating error factors, S 0 , etc., and added to obtain a total which is applied to threshold detector Sw. Operation of switch S is made, to switch Kalman filters, when said threshold value is exceeded.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19742453846 DE2453846C2 (en) | 1974-11-13 | 1974-11-13 | ARRANGEMENT FOR FAST DETECTION OF FLIGHT MANEUVERS |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1535338A true GB1535338A (en) | 1978-12-13 |
Family
ID=5930742
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB4682975A Expired GB1535338A (en) | 1974-11-13 | 1975-11-13 | Radar systems |
Country Status (3)
| Country | Link |
|---|---|
| DE (1) | DE2453846C2 (en) |
| FR (1) | FR2291504A1 (en) |
| GB (1) | GB1535338A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2214749A (en) * | 1988-01-29 | 1989-09-06 | Marconi Co Ltd | Radar seeker transient suppressor |
| GB2220812A (en) * | 1980-03-20 | 1990-01-17 | Messerschmitt Boelkow Blohm | Aerial combat director |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4144571A (en) * | 1977-03-15 | 1979-03-13 | E-Systems, Inc. | Vehicle guidance system |
| US4495580A (en) * | 1981-03-30 | 1985-01-22 | E-Systems, Inc. | Navigation system |
| JPS59191608A (en) * | 1983-04-11 | 1984-10-30 | ロツクウエル・インタ−ナシヨナル・コ−ポレ−シヨン | Improvement in processing through put speed |
| US4910526A (en) * | 1987-05-18 | 1990-03-20 | Avion Systems, Inc. | Airborne surveillance method and system |
-
1974
- 1974-11-13 DE DE19742453846 patent/DE2453846C2/en not_active Expired
-
1975
- 1975-11-12 FR FR7534466A patent/FR2291504A1/en active Granted
- 1975-11-13 GB GB4682975A patent/GB1535338A/en not_active Expired
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2220812A (en) * | 1980-03-20 | 1990-01-17 | Messerschmitt Boelkow Blohm | Aerial combat director |
| GB2220812B (en) * | 1980-03-20 | 1990-06-20 | Messerschmitt Boelkow Blohm | A combat flight director system |
| GB2214749A (en) * | 1988-01-29 | 1989-09-06 | Marconi Co Ltd | Radar seeker transient suppressor |
| US4991794A (en) * | 1988-01-29 | 1991-02-12 | The Marconi Company Limited | Radar seeker transient suppressor |
| GB2214749B (en) * | 1988-01-29 | 1992-02-19 | Marconi Co Ltd | Radar seeker transient suppressor |
Also Published As
| Publication number | Publication date |
|---|---|
| DE2453846B1 (en) | 1976-01-29 |
| FR2291504A1 (en) | 1976-06-11 |
| DE2453846C2 (en) | 1976-09-09 |
| FR2291504B1 (en) | 1977-12-16 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed | ||
| PCNP | Patent ceased through non-payment of renewal fee |