WO2006024754A1 - Procede et dispositif pour la realisation d’une liaison optique par eclats lumineux - Google Patents
Procede et dispositif pour la realisation d’une liaison optique par eclats lumineux Download PDFInfo
- Publication number
- WO2006024754A1 WO2006024754A1 PCT/FR2005/001972 FR2005001972W WO2006024754A1 WO 2006024754 A1 WO2006024754 A1 WO 2006024754A1 FR 2005001972 W FR2005001972 W FR 2005001972W WO 2006024754 A1 WO2006024754 A1 WO 2006024754A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- capacitors
- capacitor
- circuit branches
- additional capacitor
- generator
- 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.)
- Ceased
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
- G01S3/00—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic or electromagnetic waves, or particle emission, not having a directional significance, are being received
- G01S3/78—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic or electromagnetic waves, or particle emission, not having a directional significance, are being received using electromagnetic waves other than radio waves
- G01S3/782—Systems for determining direction or deviation from predetermined direction
- G01S3/783—Systems for determining direction or deviation from predetermined direction using amplitude comparison of signals derived from static detectors or detector systems
- G01S3/784—Systems for determining direction or deviation from predetermined direction using amplitude comparison of signals derived from static detectors or detector systems using a mosaic of detectors
Definitions
- the present invention relates to a method and a device for producing an optical link by flashing light between a strobe lamp and a receiver of said light flashes, which is particularly suitable for use in missile locating and guiding devices. , such as for example that described in US-4,710,028 (FR-2,583,523).
- the flashlamp may be mounted on board said missile or be arranged at a fixed station, the optical link then having a mirror mounted on board the missile and returning said light flashes to said receiver.
- Such a flashlamp must be vo ⁇ luminous and be provided with means able to evacuate to the outside the heat of which it is the seat.
- the object of the present invention is to remedy these drawbacks by making it possible to produce an optical link by means of low power consumption light bursts with a bulky flash lamp that does not require any heat dissipation.
- the method for producing an optical link, formed by a sequence of light flashes, between a flashlamp and a device for locating a mobile moving away from said disposi ⁇ tif location, each luminous flash being generated by an electric discharge produced by capacitive means and applied to said flashlamp is remarkable in that: said capacitive means is provided in the form of an arrangement of a plurality of capacitors; and in said arrangement, the branching of said capacitors is programmed so that the resulting capacitance of said capacitive means increases from one brightness to the next.
- the present invention it is possible to modulate the power of said flashlamp as a function of time so that it is reduced, when the mobile is close to the locating device, and increases progressively with the distance lamp flash-localization device, the power required for the maximum range of the mobile being provided at the end of range.
- Such a modulation thus reduces the consumption of energy by the strobe lamp, which makes it possible to reduce its heating and therefore the volume.
- said capacitive means comprise a plurality of circuit branches each comprising a capacitor and a controlled interrupter, said circuit branches being mounted in parallel on each other between the anode and the cathode of said strobe lamp, and that, on the other hand, the device comprises:
- a high voltage generator for supplying said condensa ⁇ tors; and control means of said controlled switches permitting both on the one hand to charge said capacitors from said high voltage generator and, on the other hand, to discharge said condensa ⁇ tors in said flashlamp so that the electric discharge corresponding to a burst is greater than the electric discharge corresponding to the previous brightness and lower than the electric discharge corresponding to the following brightness.
- said capacitive means comprise an additional condensa ⁇ tor mounted in parallel on said circuit branches en ⁇ be the anode and the cathode of said flashlamp.
- the capacitors of said circuit branches having different capaci ⁇ tees and, from the first to the last, are classified in order of ca ⁇ increasing capacitance; the additional capacitor has a capacitance lower than that of said first capacitor having the smallest capacitance among the capacitors of said circuit branches; the first burst of the result results from the discharge of the only additional capacitor; the second flash of the sequence results from the joint discharge of said additional capacitor and said first capacitor of said circuit branches; the third burst of the result results from the joint discharge of said additional capacitor and said first and second condensa ⁇ tors of said branches of the circuit; in general, the intermediate brightness of rank i of the sequence (i being an integer less than the total number of chips in the sequence) results from the joint discharge of said additional capacitor and i-1 first capacitors of said circuit branches ; and the last flash of the
- the device according to the present invention comprises means programmed according to the stroke of said mobile, driving said control means of said controlled switches and determining the time space between two successive flashes.
- control means are initialized, possibly with delay, by the departure of said mobile.
- the space of time between two successive flashes of light can be fixed and the same for all the flashes of the suite. However, it may be variable, for example according to an exponential law.
- the device according to the invention comprises a very high voltage generator for supplying said de-interlocking electrode and this generator is controlled by said control means of said switches.
- Figure 1 schematically illustrates the location of a missile.
- FIG. 2 is a block diagram of an exemplary embodiment of the light pulse transmitter mounted on board said missile.
- FIG. 1 shows a device 1 capable of locating a missile 2 with respect to a reference axis XX (for example a sighting axis), said missile 2 moving away at a constant speed from the locating device 1 .
- XX for example a sighting axis
- the latter is for example of the type described in US-4,710,028 (FR-2,583,523).
- the missile 2 comprises a flashlight 3, adapted to emit light pulses 4 di ⁇ rection of said device 1, which comprises a receiver of said pulses (not otherwise shown).
- the flashlamp 3 comprises a cathode 5 connected to ground, an anode 6 fed by a control device 7 and a triggering electrode 8 powered by a very high voltage generator 9 (for example). example of the order of 10 kv).
- the flashlamp has a cavity 10 forming a reflector January 1 and closed by an optical window 12.
- the cavity 10 is filled with a rare gas, for example xenon.
- the capacitive means 13 comprise five capacitors C1 to C5 connected in parallel, the anodes of said capacitors being connected in common on the one hand to the high voltage generator 14 and, on the other hand, on the other hand, at the anode 6 of the flashlamp 3.
- the cathode of the capacitor C1 is connected directly to the ground, whereas the cathodes of the capacitors C2 to C5 are respectively connected to ground via switches 12 to 15 (for example MOS transistors), controlled by the control device 15.
- switches 12 to 15 for example MOS transistors
- the capacitance of the capacitor C5 is greater than that of the capacitor C4, which itself is greater than that of the capacitor C3, which itself is greater than the capacitance of the capacitor C2, which itself is greater than that of the capacitor C1.
- the capacitances c2 to c5 of the capacitors C2 to C5 may be respectively equal to 2c1, 3c1, 4c1 and 5c1. Since the capacitor C1 is in permanent connection with the generator 14, it is charged by the latter.
- a control command is sent to the programmed tops generator 16 by a command line 18, on la ⁇ which may optionally be interposed a timing device (not shown).
- the generator 16 drives the device 15 to close the switches 12 to 15, so that the capacitors C2 to C5 are loaded by the generator 14.
- a switch has been closed he remains in this state.
- the generator 16 emits a first top which is addressed to the control device 15. This activates the very high voltage generator 9, so that the trigger electrode 8 is por ⁇ ted to this very high tension. Since, moreover, the voltage at the terminals of the capacitor C1 is applied between the cathode 5 and the anode 6, it follows the generation of an electric arc between the latter, as well as the discharge of said capacitor C1. The power of this short arc, which forms a first luminous flash, is therefore proportional to the electrical charge accumulated in the single capacitor C1, which itself is a function of the capacitance of this capacitor C1. At the end of said first light burst, the control device 15, driven by the generator 16, deactivates the very high voltage generator 9 and closes the switch 12, so that the capacitors C1 and C2 are recharged by the generator 14;
- the generator 16 emits a second top and the control device 15, which receives it, activates the generator of very high voltage 9. It follows that the lamp 3 engen ⁇ dre a second luminous glow whose power is proportional to the sum of the electrical charges accumulated in the capacitors C1 and C2. At the end of the second luminous flash, the control device 1 5 deactivates the very high voltage generator 9 and closes the switch 13.
- the lamp 3 generates a third luminous flash whose power is proportional to the sum of ac ⁇ accumulated electrical charges in the capacitors C1, C2 and C3.
- the control device 1 5 driven by the generator 1 6, deactivates the very high voltage generator 9 and closes the interrup ⁇ tor 14.
- the lamp 3 generates a fifth luminous brightness of which the power is proportional to the sum of the electrical charges accumulated in the capacitors CI, C2, C3, C4 and C5.
- the instants t1 to t5 and the time spaces ⁇ t1 to ⁇ t4 are programmed in the generator 16. Said spaces ⁇ t1 to ⁇ t4 can be constant and equal. On the contrary, they can be variable.
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- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Discharge-Lamp Control Circuits And Pulse- Feed Circuits (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Optical Couplings Of Light Guides (AREA)
- Optical Integrated Circuits (AREA)
- Non-Portable Lighting Devices Or Systems Thereof (AREA)
- Manufacture, Treatment Of Glass Fibers (AREA)
- Blinds (AREA)
Abstract
Description
Claims
Priority Applications (6)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2007526505A JP4538051B2 (ja) | 2004-08-20 | 2005-07-28 | 光閃光を用いて光学リンクを作成する方法と装置 |
| CN2005800285927A CN101006320B (zh) | 2004-08-20 | 2005-07-28 | 利用闪光产生光链的方法和装置 |
| KR1020077006027A KR101141318B1 (ko) | 2004-08-20 | 2005-07-28 | 광 플래시를 이용하여 광학 링크를 생성하기 위한 방법 및장치 |
| US11/573,821 US7582853B2 (en) | 2004-08-20 | 2005-07-28 | Method and device for producing an optical link using light flashes |
| IL179193A IL179193A (en) | 2004-08-20 | 2006-11-12 | Method and device for producing an optical link using light flashes |
| NO20071457A NO337391B1 (no) | 2004-08-20 | 2007-03-19 | Fremgangsmåte og innretning for å produsere en optisk link ved å benytte lysblink |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0409014A FR2874434B1 (fr) | 2004-08-20 | 2004-08-20 | Procede et dispositif pour la realisation d'une liaison optique par eclats lumineux |
| FR0409014 | 2004-08-20 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| WO2006024754A1 true WO2006024754A1 (fr) | 2006-03-09 |
| WO2006024754A9 WO2006024754A9 (fr) | 2006-04-20 |
Family
ID=34948286
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/FR2005/001972 Ceased WO2006024754A1 (fr) | 2004-08-20 | 2005-07-28 | Procede et dispositif pour la realisation d’une liaison optique par eclats lumineux |
Country Status (12)
| Country | Link |
|---|---|
| US (1) | US7582853B2 (fr) |
| EP (1) | EP1628111B1 (fr) |
| JP (1) | JP4538051B2 (fr) |
| KR (1) | KR101141318B1 (fr) |
| CN (1) | CN101006320B (fr) |
| AT (1) | ATE412875T1 (fr) |
| DE (1) | DE602005010637D1 (fr) |
| FR (1) | FR2874434B1 (fr) |
| IL (1) | IL179193A (fr) |
| NO (1) | NO337391B1 (fr) |
| WO (1) | WO2006024754A1 (fr) |
| ZA (1) | ZA200610634B (fr) |
Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8916809B2 (en) * | 2003-08-12 | 2014-12-23 | Omnitek Partners Llc | Projectile having a window for transmitting power and/or data into the projectile interior |
| FR2908874B1 (fr) * | 2006-11-21 | 2009-01-23 | Mbda France Sa | Systeme de visee a ecartometre integre. |
| US8082832B1 (en) * | 2007-05-14 | 2011-12-27 | Lockheed Martin Corporation | Missile system using two-color missile-signature simulation using mid-infrared test source semiconductor lasers |
| US8692889B2 (en) * | 2010-03-17 | 2014-04-08 | Drs Rsta, Inc. | Image magnitude differential based system and method for tracking cooperative, non-incandescent sources |
| US10062910B2 (en) * | 2010-05-27 | 2018-08-28 | Omnitek Partners Llc | Reserve power source for munitions |
| US20120206084A1 (en) * | 2010-05-27 | 2012-08-16 | Omnitek Partners Llc | Reserve Power Source for Munitions |
| US20140210273A1 (en) * | 2010-05-27 | 2014-07-31 | Omnitek Partners Llc | Hybrid Reserve Power Source Systems For Munitions |
| US8668010B2 (en) | 2010-12-06 | 2014-03-11 | Halliburton Energy Services, Inc. | Wellbore servicing compositions comprising a fluid loss agent and methods of making and using same |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2274887A1 (fr) * | 1974-08-28 | 1976-01-09 | Bofors Ab | Appareil de regulation de la puissance d'un faisceau dit de guidage optique |
| US4173777A (en) * | 1977-06-01 | 1979-11-06 | Cincinnati Electronics Corporation | Jet aircraft and/or missile plume simulator |
| FR2583523A1 (fr) * | 1985-06-17 | 1986-12-19 | Aerospatiale | Systeme pour la localisation d'un mobile. |
| US5062586A (en) * | 1990-05-17 | 1991-11-05 | Electronics & Space Corporation | Missile tracking, guidance and control apparatus |
| US5332176A (en) * | 1992-12-03 | 1994-07-26 | Electronics & Space Corp. | Controlled interlace for TOW missiles using medium wave infrared sensor or TV sensor |
| US20020154293A1 (en) * | 2001-04-19 | 2002-10-24 | Wells Michael L. | Solid state modulated beacon tracking system |
| WO2004064274A1 (fr) * | 2002-12-10 | 2004-07-29 | Mbda France | Procede et dispositif pour la realisation d'une liaison optique par impulsions laser |
Family Cites Families (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5350134A (en) * | 1973-07-03 | 1994-09-27 | Gec Ferranti Defence Systems Limited | Target identification systems |
| US6078606A (en) * | 1975-03-17 | 2000-06-20 | Lockheed Martin Corporation | Multi-color, multi-pulse laser |
| US4179085A (en) * | 1978-01-03 | 1979-12-18 | The United States Of America As Represented By The Secretary Of The Army | Optical boresight method for nutating system |
| US4419012A (en) * | 1979-09-11 | 1983-12-06 | Elliott Brothers (London) Limited | Position measuring system |
| US4424943A (en) * | 1981-05-04 | 1984-01-10 | Hughes Aircraft Company | Tracking system |
| US4600305A (en) * | 1984-08-20 | 1986-07-15 | The United States Of America As Represented By The Secretary Of The Army | Dynamic energy centroid locator and processor (declp) |
| US5147088A (en) * | 1986-04-29 | 1992-09-15 | British Aerospace Public Limited Company | Missile tracking systems |
| FR2653562B1 (fr) * | 1989-10-23 | 1992-02-28 | Aerospatiale | Systeme pour la localisation d'un mobile. |
| JP3213335B2 (ja) * | 1991-05-15 | 2001-10-02 | 松下電工株式会社 | 光源点灯装置 |
| FR2733326B1 (fr) * | 1995-04-24 | 1997-06-06 | Aerospatiale | Systeme pour determiner la position et l'angle de roulis d'un mobile |
| US5651512A (en) * | 1995-09-28 | 1997-07-29 | Hughes Electronics | Missile tracking system with a thermal track link |
| JP3599313B2 (ja) * | 1998-12-15 | 2004-12-08 | 株式会社リコー | ネットワークファクシミリ装置およびその制御方法 |
| FR2857088B1 (fr) * | 2003-07-04 | 2005-09-16 | Mbda France | Missile tournant emettant des impulsions lumineuses. |
-
2004
- 2004-08-20 FR FR0409014A patent/FR2874434B1/fr not_active Expired - Lifetime
-
2005
- 2005-07-28 CN CN2005800285927A patent/CN101006320B/zh not_active Expired - Fee Related
- 2005-07-28 DE DE602005010637T patent/DE602005010637D1/de not_active Expired - Lifetime
- 2005-07-28 JP JP2007526505A patent/JP4538051B2/ja not_active Expired - Fee Related
- 2005-07-28 AT AT05291608T patent/ATE412875T1/de not_active IP Right Cessation
- 2005-07-28 WO PCT/FR2005/001972 patent/WO2006024754A1/fr not_active Ceased
- 2005-07-28 KR KR1020077006027A patent/KR101141318B1/ko not_active Expired - Fee Related
- 2005-07-28 US US11/573,821 patent/US7582853B2/en not_active Expired - Lifetime
- 2005-07-28 EP EP05291608A patent/EP1628111B1/fr not_active Expired - Lifetime
-
2006
- 2006-11-12 IL IL179193A patent/IL179193A/en active IP Right Grant
- 2006-12-18 ZA ZA200610634A patent/ZA200610634B/en unknown
-
2007
- 2007-03-19 NO NO20071457A patent/NO337391B1/no unknown
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2274887A1 (fr) * | 1974-08-28 | 1976-01-09 | Bofors Ab | Appareil de regulation de la puissance d'un faisceau dit de guidage optique |
| US4173777A (en) * | 1977-06-01 | 1979-11-06 | Cincinnati Electronics Corporation | Jet aircraft and/or missile plume simulator |
| FR2583523A1 (fr) * | 1985-06-17 | 1986-12-19 | Aerospatiale | Systeme pour la localisation d'un mobile. |
| US5062586A (en) * | 1990-05-17 | 1991-11-05 | Electronics & Space Corporation | Missile tracking, guidance and control apparatus |
| US5332176A (en) * | 1992-12-03 | 1994-07-26 | Electronics & Space Corp. | Controlled interlace for TOW missiles using medium wave infrared sensor or TV sensor |
| US20020154293A1 (en) * | 2001-04-19 | 2002-10-24 | Wells Michael L. | Solid state modulated beacon tracking system |
| WO2004064274A1 (fr) * | 2002-12-10 | 2004-07-29 | Mbda France | Procede et dispositif pour la realisation d'une liaison optique par impulsions laser |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2006024754A9 (fr) | 2006-04-20 |
| IL179193A (en) | 2012-04-30 |
| US7582853B2 (en) | 2009-09-01 |
| IL179193A0 (en) | 2007-03-08 |
| NO337391B1 (no) | 2016-04-04 |
| EP1628111B1 (fr) | 2008-10-29 |
| CN101006320B (zh) | 2010-06-02 |
| JP2008510951A (ja) | 2008-04-10 |
| ZA200610634B (en) | 2007-12-27 |
| US20080018264A1 (en) | 2008-01-24 |
| KR20070048787A (ko) | 2007-05-09 |
| EP1628111A1 (fr) | 2006-02-22 |
| FR2874434B1 (fr) | 2006-11-17 |
| DE602005010637D1 (de) | 2008-12-11 |
| FR2874434A1 (fr) | 2006-02-24 |
| NO20071457L (no) | 2007-05-18 |
| JP4538051B2 (ja) | 2010-09-08 |
| ATE412875T1 (de) | 2008-11-15 |
| KR101141318B1 (ko) | 2012-05-04 |
| CN101006320A (zh) | 2007-07-25 |
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