DE3501955A1 - Target-search method for a terminally-guided munition - Google Patents
Target-search method for a terminally-guided munitionInfo
- Publication number
- DE3501955A1 DE3501955A1 DE19853501955 DE3501955A DE3501955A1 DE 3501955 A1 DE3501955 A1 DE 3501955A1 DE 19853501955 DE19853501955 DE 19853501955 DE 3501955 A DE3501955 A DE 3501955A DE 3501955 A1 DE3501955 A1 DE 3501955A1
- Authority
- DE
- Germany
- Prior art keywords
- target
- ammunition
- seeker
- radar
- signal
- 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.)
- Granted
Links
Classifications
-
- 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
- F41G7/22—Homing guidance systems
- F41G7/2233—Multimissile systems
Landscapes
- Engineering & Computer Science (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)
Abstract
Description
Siemens Aktiengesellschaft Unser Zeichen Berlin und München VPA 85 P 1 0 2 5 DESiemens Aktiengesellschaft Our symbol Berlin and Munich VPA 85 P 1 0 2 5 DE
Zielsuchverfahren für endphasengelenkte MunitionTarget seeking method for end-phase guided ammunition
Die Erfindung bezieht sich auf ein Zielsuchverfahren für endphasengelenkte Munition, bei der mehrere, jeweils mit einem Radarzielsuchkopf versehene Tochtermunitionen (Lenkflugkörper) aus einem Behälter über dem Zielgebiet ausgestoßen werden.The invention relates to a target search method for end-phase guided ammunition, in which several, each with daughter ammunition (guided missile) provided with a radar seeker head from a container above the target area be expelled.
Bei der Verteilung der Tochtermunitionen auf die einzelnen Ziele verläßt man sich hierbei - soweit bekannt - auf die natürliche Streuung der ausgestoßenen Tochtermunitionen. Es läßt sich durch diese Art von Verteilung jedoch nicht verhindern, daß manchmal doch mehrere Tochtermunitionen dasselbe Ziel verfolgen, was zum einen eine Verschwendung von Munition und damit verbundenen Suchköpfen, zum anderen aber auch dazu führen kann, daß manche Ziele wegen der Mehrfachbeaufschlagung anderer Ziele überhaupt nicht angesteuert werden und deshalb entkommen können.When it comes to distributing the subsidiary ammunition to the individual targets, one relies on it - so far known - on the natural dispersion of the ejected daughter ammunition. It can be done through this type of distribution but not prevent that sometimes several daughter ammunitions pursue the same goal, what on the one hand a waste of ammunition and the associated search heads, on the other hand it is also a waste of ammunition can lead to the fact that some targets are not approached at all because of the multiple application of other targets and therefore can escape.
Aufgabe der Erfindung ist es, ein Zielsuchverfahren der eingangs genannten Art so auszubilden, daß die Aufschaltung mehrerer Tochtermunitionen (Lenkflugkörper) auf ein einziges Ziel verhindert wird.The object of the invention is to develop a target search method of the type mentioned at the outset in such a way that the connection multiple daughter ammunition (guided missile) on a single target is prevented.
Gemäß der Erfindung wird diese Aufgabe dadurch gelöst, daß in einem Signalempfänger jedes Radarzielsuchkopfes die vom gerade verfolgten Ziel reflektierte Strahlung daraufhin analysiert wird, ob das von einem anderen Zielsuchkopf ausgesendete Signal, welches sich vom Signal des eigenen Radarsenders unterscheiden kann,According to the invention, this object is achieved in that each radar target seeker head in a signal receiver The radiation reflected from the target being pursued is analyzed to determine whether it is from someone else Target seeker emitted signal, which can differ from the signal of the own radar transmitter,
VL 1 Mai /17.01.85 6 AusfertigungenVL 1 May / 17.01.85 6 copies
f·Ausfertigung f · Execution
-2- VPA SS P 1 0 2 5 DE-2- VPA SS P 1 0 2 5 DE
darin enthalten ist oder nicht und daß sich jeder Radarzielsuchkopf und somit auch jede damit verbundene Tochtermunition für denjenigen Fall, in dem das Signal eines anderen Zielsuchkopfes bereits im analysierten Echosignal enthalten ist, ein anderes Ziel zur Verfolgung sucht.is contained therein or not and that each radar target seeker head and thus each associated with it Daughter ammunition for those cases in which the signal from another homing head is already being analyzed Echo signal is contained, is looking for another target to pursue.
Ein Zielsuchkopf verfolgt also nur dann ein von ihm erfaßtes Ziel weiter, wenn dieses nicht bereits vom Sendesignal des Zielsuchkopfes einer anderen Tochtermunition beaufschlagt wird. Falls möglich, sollte aus Einsparungsgründen die Zahl der über dem Zielgebiet ausgestoßenen Tochtermunitionen der Anzahl der in diesem Zielgebiet zu erfassenden Ziele entsprechen.A target seeker therefore only continues to pursue a target it has detected if it is not already from Transmission signal of the homing head of another daughter ammunition is applied. If possible, in order to save money, the number of over the target area daughter munitions emitted correspond to the number of targets to be recorded in this target area.
Damit keine zeitliche Verwirrung eintritt, kann in zweckmäßiger Weise vorgesehen werden, daß die Sender der ι einzelnen Tochtermunitionen zeitlich nacheinander eingeschaltet werden, so daß jeder Suchkopf schon ein *Thus no time confusion occurs, may be provided in an expedient manner that the transmitters of the individual subsidiary ι munitions are turned on sequentially in time such that each seeker ever *
bestimmtes Ziel ausgewählt hat, bevor der nächste Suchkopf einschaltet.selected target before the next seeker turns on.
2 Patentansprüche
252 claims
25th
Claims (2)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19853501955 DE3501955A1 (en) | 1985-01-22 | 1985-01-22 | Target-search method for a terminally-guided munition |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19853501955 DE3501955A1 (en) | 1985-01-22 | 1985-01-22 | Target-search method for a terminally-guided munition |
Publications (2)
Publication Number | Publication Date |
---|---|
DE3501955A1 true DE3501955A1 (en) | 1986-07-24 |
DE3501955C2 DE3501955C2 (en) | 1987-10-01 |
Family
ID=6260419
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19853501955 Granted DE3501955A1 (en) | 1985-01-22 | 1985-01-22 | Target-search method for a terminally-guided munition |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE3501955A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3531008A1 (en) * | 1985-08-30 | 1987-03-12 | Dynamit Nobel Ag | Target-seeking missile |
US8288698B2 (en) | 2009-06-08 | 2012-10-16 | Rheinmetall Air Defence Ag | Method for correcting the trajectory of terminally guided ammunition |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4394997A (en) * | 1980-04-14 | 1983-07-26 | General Dynamics, Pomona Division | Sequential time discrimination system for sub-delivery systems |
-
1985
- 1985-01-22 DE DE19853501955 patent/DE3501955A1/en active Granted
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4394997A (en) * | 1980-04-14 | 1983-07-26 | General Dynamics, Pomona Division | Sequential time discrimination system for sub-delivery systems |
Non-Patent Citations (1)
Title |
---|
Z.: Flight International 8. Jan. 1983, S. 91-93 * |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3531008A1 (en) * | 1985-08-30 | 1987-03-12 | Dynamit Nobel Ag | Target-seeking missile |
US8288698B2 (en) | 2009-06-08 | 2012-10-16 | Rheinmetall Air Defence Ag | Method for correcting the trajectory of terminally guided ammunition |
Also Published As
Publication number | Publication date |
---|---|
DE3501955C2 (en) | 1987-10-01 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
OP8 | Request for examination as to paragraph 44 patent law | ||
D2 | Grant after examination | ||
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |