GB1377358A - Method of advancing the point of impact for passive-location missiles guided by means of proportional navigation in the self-guide phase - Google Patents
Method of advancing the point of impact for passive-location missiles guided by means of proportional navigation in the self-guide phaseInfo
- Publication number
- GB1377358A GB1377358A GB4053968A GB4053968A GB1377358A GB 1377358 A GB1377358 A GB 1377358A GB 4053968 A GB4053968 A GB 4053968A GB 4053968 A GB4053968 A GB 4053968A GB 1377358 A GB1377358 A GB 1377358A
- Authority
- GB
- United Kingdom
- Prior art keywords
- impact
- point
- torpedo
- injected
- term
- 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
- 208000004350 Strabismus Diseases 0.000 abstract 2
- 230000003321 amplification Effects 0.000 abstract 1
- 238000006073 displacement reaction Methods 0.000 abstract 1
- 238000003199 nucleic acid amplification method Methods 0.000 abstract 1
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
- F41G7/2273—Homing guidance systems characterised by the type of waves
- F41G7/228—Homing guidance systems characterised by the type of waves using acoustic waves, e.g. for torpedoes
-
- 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
- F41G7/2213—Homing guidance systems maintaining the axis of an orientable seeking head pointed at the target, e.g. target seeking gyro
-
- 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
- F41G7/2253—Passive homing systems, i.e. comprising a receiver and do not requiring an active illumination of the target
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/12—Target-seeking control
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Acoustics & Sound (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Navigation (AREA)
Abstract
1377358 Automatic control of course LICENTIA PATENT-VERWALTUNGS-GmbH 23 Aug 1968 [14 Oct 1967] 40539/68 Heading G3R In a torpedo proportional navigation control system, the control is effected initially along a wire and in the final phase is effected by a self guidance device, mounted on the torpedo and operated acoustically. To prevent the torpedo aiming directly at the noise source, (the propeller wake) the point of impact with the target ship is advanced from the stern of the ship. Control of the missile is effected with regard to angular bearing rates of charge and to produce the displacement of the impact point, a term is injected into the control system for a predetermined interval, so as to produce an angle-of-squint track. In switching from the proportional navigation to the angle-of-squint the amplification factor of the guide system is set to unity and the injected term is applied for an interval which is a function of the amplitude of the time variation of the injected term.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE1967L0057648 DE1578299B2 (en) | 1967-10-14 | 1967-10-14 | PROCEDURE FOR RETAINING THE MEETING POINT FOR PASSIVE LOCATIONS IN THE SELF-STEERING PHASE USING PROPORTIONAL NAVIGATION OF JOINTED SHELVES |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1377358A true GB1377358A (en) | 1974-12-11 |
Family
ID=7278714
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4053968A Expired GB1377358A (en) | 1967-10-14 | 1968-08-23 | Method of advancing the point of impact for passive-location missiles guided by means of proportional navigation in the self-guide phase |
Country Status (4)
Country | Link |
---|---|
DE (1) | DE1578299B2 (en) |
FR (1) | FR1605394A (en) |
GB (1) | GB1377358A (en) |
IT (1) | IT989554B (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2421423A1 (en) * | 1978-03-31 | 1979-10-26 | Ibm | CONNECTION CONTROL DEVICE IN A DATA PROCESSING SYSTEM |
FR2594538A1 (en) * | 1986-02-14 | 1987-08-21 | Thomson Csf | Method for measuring deviations in setting between the reference trihedron of an inertial unit and an external reference trihedron, and its use in a weapons system |
EP1798622A1 (en) * | 2005-12-19 | 2007-06-20 | NEXTER Munitions | Method providing the navigation and/or guidance of a projectile towards a target and device implementing said method |
CN115047877A (en) * | 2022-06-08 | 2022-09-13 | 中国船舶集团有限公司系统工程研究院 | Unmanned ship target tracking method and system based on proportional guidance |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2824059C2 (en) * | 1973-05-12 | 1986-11-13 | Bodenseewerk Gerätetechnik GmbH, 7770 Überlingen | Control device for the final phase control of projectiles |
DE2918128C1 (en) * | 1979-05-07 | 1988-11-10 | Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt, De | |
DE3048272C2 (en) * | 1980-12-20 | 1983-03-24 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Guidance method for ammunition |
DE3918701A1 (en) * | 1989-06-08 | 1990-12-13 | Diehl Gmbh & Co | METHOD FOR IMPROVING THE ACCURACY OF A PROGRAMMED FLYING BODY |
-
1967
- 1967-10-14 DE DE1967L0057648 patent/DE1578299B2/en active Granted
-
1968
- 1968-08-23 GB GB4053968A patent/GB1377358A/en not_active Expired
- 1968-09-12 IT IT39713/68A patent/IT989554B/en active
-
1969
- 1969-09-27 FR FR167949A patent/FR1605394A/fr not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2421423A1 (en) * | 1978-03-31 | 1979-10-26 | Ibm | CONNECTION CONTROL DEVICE IN A DATA PROCESSING SYSTEM |
FR2594538A1 (en) * | 1986-02-14 | 1987-08-21 | Thomson Csf | Method for measuring deviations in setting between the reference trihedron of an inertial unit and an external reference trihedron, and its use in a weapons system |
EP1798622A1 (en) * | 2005-12-19 | 2007-06-20 | NEXTER Munitions | Method providing the navigation and/or guidance of a projectile towards a target and device implementing said method |
FR2895099A1 (en) * | 2005-12-19 | 2007-06-22 | Giat Ind Sa | METHOD FOR PROVIDING NAVIGATION AND / OR GUIDANCE AND / OR CONTROL OF A PROJECTILE TO A GOAL AND DEVICE IMPLEMENTING SUCH A METHOD |
CN115047877A (en) * | 2022-06-08 | 2022-09-13 | 中国船舶集团有限公司系统工程研究院 | Unmanned ship target tracking method and system based on proportional guidance |
CN115047877B (en) * | 2022-06-08 | 2024-06-07 | 中国船舶集团有限公司系统工程研究院 | Unmanned ship target tracking method and system based on proportional guidance |
Also Published As
Publication number | Publication date |
---|---|
IT989554B (en) | 1975-06-10 |
DE1578299B2 (en) | 1976-03-11 |
DE1578299A1 (en) | 1975-03-20 |
FR1605394A (en) | 1975-02-28 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] |