EP1135876A1 - Terminal reconfigurable pour communications laser - Google Patents

Terminal reconfigurable pour communications laser

Info

Publication number
EP1135876A1
EP1135876A1 EP99971229A EP99971229A EP1135876A1 EP 1135876 A1 EP1135876 A1 EP 1135876A1 EP 99971229 A EP99971229 A EP 99971229A EP 99971229 A EP99971229 A EP 99971229A EP 1135876 A1 EP1135876 A1 EP 1135876A1
Authority
EP
European Patent Office
Prior art keywords
polarization
wavelength
optical
transmitted
terminal
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.)
Withdrawn
Application number
EP99971229A
Other languages
German (de)
English (en)
Inventor
David A. Rockwell
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
DirecTV Group Inc
Original Assignee
Hughes Electronics Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Hughes Electronics Corp filed Critical Hughes Electronics Corp
Publication of EP1135876A1 publication Critical patent/EP1135876A1/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04B—TRANSMISSION
    • H04B10/00—Transmission systems employing electromagnetic waves other than radio-waves, e.g. infrared, visible or ultraviolet light, or employing corpuscular radiation, e.g. quantum communication
    • H04B10/11—Arrangements specific to free-space transmission, i.e. transmission through air or vacuum
    • H04B10/118—Arrangements specific to free-space transmission, i.e. transmission through air or vacuum specially adapted for satellite communication

Definitions

  • An optical communication terminal comprising: a transmitter (40) for generating an outbound optical signal having a first polarization and first wavelength; a receiver (48) for receiving an inbound optical signal having a second polarization and second wavelength; a polarization beamsplitter (56) operable to direct optical signals having the first polarization and either the first or second wavelength from the transmitter (40) while directing optical signals having the second polarization and either the first or second wavelength to and from the receiver (48); and a reconfigurable polarization changer (56) operable to change polarization of optical signals passing therethrough, the polarization changer (56) responsive to a command signal to select one of a first state in which output signal polarization is changed to a third polarization and at least a second state in which output signal polarization is changed to a fourth polarization.
  • first and second polarizations are perpendicular linear polarizations and the third and fourth polarizations are circular polarizations.
  • reconfigurable polarization changer (56) further comprises a positioning motor (60) for rotating the wave plate in response to the command signal.
  • reconfigurable polarization changer (56) comprises a polarization rotator.
  • the present invention relates to a reconfigurable laser communications terminal particularly suited for optical intersatellite links.
  • Optical intersatellite link terminals are utilized to communicate between two satellites.
  • One of the principal technical challenges in designing communication networks involving these terminals is to isolate the receiver channel within any terminal from back-scatter or any other spurious radiation that may be produced by the transmitted beam originating within the same optical terminal.
  • the isolation requirement is often greater than 90 dB, i.e. any spurious signal generated by the transmitter beam which can possibly enter the receiver channel must be less than the transmitter beam itself by at least 90 dB.
  • a dual- wavelength OISL network requires (at least) two types of terminals which are characterized by their operating wavelengths. For example, terminals of type A transmit radiation at a first wavelength and receive radiation at a second wavelength, while terminals of type B transmit at the second wavelength and receive at the first wavelength.
  • a successful communication link requires that an A te ⁇ ninal communicate with a B terminal.
  • the operating wavelengths are typically separated by about 5 to 10 nanometers (nm) which is large enough that -2-
  • a dichroic beamsplitter is used which reflects the first wavelength while transmitting the second wavelength.
  • a second known isolation method employs polarization-based switching techniques to isolate the transmitted and received beams which operate at the same wavelength but orthogonal polarizations. This approach provides isolation of only about 30 dB to 40 dB depending upon the particular implementation and is therefore not appropriate for many OISL applications which have more stringent isolation requirements.
  • temporal isolation i.e. transmitting and receiving at different times, represents a fourth approach that may be used to provide sufficient isolation but imposes severe constraints on the communication format that can be used. Furthermore, temporal isolation requires the system to adapt to changes in intersatellite range and is therefore undesirable.
  • the terminals of the communication system should be reconfigurable such that an A terminal can convert to a B te ⁇ ninal (and vice versa) upon receipt of an appropriate command from the network controller.
  • One approach to providing this reconfigurability is to mechanically exchange a dichroic beamsplitter so that the appropriate wavelength for the A or B terminal is directed to the receiver channel and from the transmitter.
  • this approach requires complex and costly mechanical and electronic componentry to achieve the precise alignment necessary for the repeated switches between type A and B terminals throughout the life of the satellite network.
  • Another object of the present invention is to provide a system and method for separating a transmit beam from a receive beam in a dual-wavelength optical commumcation system which exhibits similar performance characteristics for both types of terminals to facilitate reconfigurability.
  • a further object of the present invention is to provide a method for reconfiguring an optical communication terminal while reducing or eliminating mechanical motion of optical elements.
  • Yet another object of the present invention is to provide a polarization-based reconfigurable communication system and method which combine optical paths of the transmit and receive beams while improving isolation.
  • An additional object of the present invention is to provide a system and method for reconfiguring an optical communication terminal in response to a control command by exchanging transmit and receive signal types.
  • Another object of the invention is to provide a system and method for reconfiguring an optical communication terminal which reduce or eliminate repositioning of beam steering components.
  • a system and method for optical communication include at least one reconfigurable terminal using dual-wavelength operation for isolation between transmitted and received signals in combination with polarization switching to separate and steer the transmitted and received signals to and from corresponding receivers and transmitters, respectively.
  • the polarization based switching provides wavelength independent beam steering to facilitate interchanging of wavelengths for transmitted and received signals.
  • a controllable or passive polarization changer such as a wave plate or polarization rotator, in conjunction with selectable or tunable bandpass filters, allow the communication terminal to be reconfigured without also requiring the repositioning and associated precision alignment of beam steering optics.
  • an optical communication terminal includes a transmitter for generating an optical signal having a first polarization and first wavelength and a receiver for receiving an optical signal having a second polarization and second wavelength.
  • a polarization beamsplitter directs optical signals having the first polarization and first wavelength from the transmitter while directing optical signals having the second polarization and second wavelength to the receiver.
  • a reconfigurable polarization changer operable to change polarization of optical signals passing therethrough is responsive to a command signal to select one of a first state in which output signal polarization is changed from the first polarization to a third polarization (while also changing a fourth polarization to the second) and at least a second state in which output signal polarization is changed from the first polarization to the fourth polarization (while also changing the third polarization to the second polarization).
  • a method for optical communication includes transmitting optical communication signals at a fir st wavelength and first polarization, and receiving optical communication signals at a second wavelength and second polarization.
  • the transmitted and received signals travel along an optical path passing through at least one optical element common to both transmitted and received signals.
  • the first and second wavelengths are selected to provide a predetermined level of isolation between transmitted and received optical communication signals within a particular communication terminal.
  • the method also includes spatially separating transmitted signals from received signals based on the first and second polarizations but substantially independently of the first and second wavelengths, and selectively reconfiguring the commumcation terminal by interchanging the first and second wavelengths and polarizations such that optical communication signals are transmitted from the terminal at the second wavelength and second polarization and received by the terminal at the first wavelength and first polarization.
  • One embodiment of an optical communication system includes a first satellite having a first optical communication terminal transmitting optical signals at a first wavelength with a first polarization and receiving optical signals at a second wavelength and second polarization. At least one additional satellite having a second optical communication terminal transmits optical signals at the second wavelength with the second polarization and receives signals at the first wavelength and the first polarization. At least the first optical communication terminal is selectively reconfigurable to interchange transmitting and receiving wavelengths and polarizations in response to a command signal, preferably without repositioning and/or realignment of any beam steering optics.
  • the present invention provides a number of advantages for optical communication systems. For example, the present invention provides superior performance as measured by cost, size, weight, complexity, and reliability compared to other approaches.
  • the present invention accomplishes the required optical switching or beam steering function using conventional beamsplitters and avoids repositioning and associated precision alignment of beam steering optics.
  • the present invention may be implemented with commercially available polarization components enabling a low-cost solution to the switching problem while providing reconfigurable commumcation terminals to improve system flexibility and overall reliability.
  • Figure 1 is a block diagram of an optical satellite communication system according to the present invention.
  • FIG. 2 is a partial block diagram for an optical communication terminal according to the present invention.
  • Figure 3 is a flow chart illustrating a method for intersatellite optical communication according to the present invention. Best Mode For Carrying Out The Invention
  • FIG. 1 a block diagram illustrating one application for an optical communication system according to the present invention is shown.
  • the present invention is generally applicable to any free-space optical communication system with one example being a satellite-based communication system as illustrated and described in detail below.
  • the illustrative example provided below is described with reference to communication signals, the present invention is equally applicable to acquisition and tracking systems and/or subsystems which also require transmitting and receiving signals that often utilize common optics and must address the same isolation challenges described above. -8-
  • Satellite communication system 10 includes a number of satellites 12, 14 in orbit about the Earth 16. Satellites 12, 14 include one or more optical communication terminals 18 which may perform free-space optical communication according to the present invention. Satellites 12, 14 also include directional communication systems for transmitting information to ground station 20 via downlink 22 which is typically an RF link. Likewise, ground station 20 may communicate data including control commands to satellites 12, 14 via uplink 24.
  • Communication system 10 is preferably a dual-wavelength system which incorporates at least two types of terminals 18 characterized by their selected operating wavelengths.
  • terminals 26 referred to as type
  • a successful communication link requires that an "A" terminal communicate with a "B" terminal.
  • the two operating wavelengths are typically separated by 5 to 10 nanometers. This is large enough for readily available receiver bandpass filters to adequately reject transmitter radiation while providing the required isolation, typically 90dB.
  • the two satellites preferably transmit and receive communication signals along a common line-of-sight, or communication beam axis, which is illustrated as separate transmit and receive beams in Figure 1 for clarity and ease of description only.
  • a beam or signal is “transmitted” when it leaves the communication terminal and “received” when it arrives at the communication terminal.
  • a transmitter "generates” a signal or beam -9-
  • the generated signal or beam passes through various optical elements within the communication terminal, including a polarization changer, such that the transmitted beam is characterized by the same wavelength but a different polarization relative to the generated beam.
  • a "received" signal having an associated wavelength and polarization passes through the polarization changer within the commumcation terminal prior where it is referred to as a "detected" signal or beam which passes to the receiver.
  • the "detected" beam or signal will have the same wavelength, but a different polarization, relative to the "received” beam which arrives at the communication terminal.
  • redundant communication terminals may be included to compensate for those terminals which deteriorate or become inoperable during the desired lifetime.
  • This strategy is most prevalent in satellite-based systems since repair or replacement of a terminal is very difficult or impossible.
  • a sufficient number of terminals of complementary types must be present to maintain the required links.
  • the present invention provides one or more reconfigurable terminals 30 to reduce the number of required terminals as explained in greater detail below.
  • satellite 12 includes a first optical communication terminal 26 which transmits optical signals at a first wavelength ⁇ ⁇ with a first polarization Pj and receives optical signals at a second wavelength ⁇ 2 and second polarization P 2 .
  • Satellite 14 preferably includes a second optical communication terminal 28 which transmits optical signals at the second wavelength ⁇ 2 with the second polarization P 2 .
  • Communication terminal 28 receives signals at the first wavelength ⁇ j with the first polarization P t .
  • Optical communication terminal 30 is selectively reconfigurable to interchange transmitting ⁇ 10-
  • Satellite 14 may also include various other optical communication terminals 18 which transmit optical signals at the first wavelength ⁇ , and first polarization P ⁇
  • satellite 12 may also include various other optical communication terminals which transmit optical signals at the second wavelength ⁇ 2 and second polarization P 2
  • FIG 2 a partial block diagram of an optical communication terminal according to the present invention is shown.
  • this block diagram includes only those elements which facilitate description of the present invention and that any actual implementation may include additional elements and/or equivalent elements without departing from the spirit or scope of the present invention.
  • the present invention may be implemented with discrete commercially available components, custom integrated components, or any combination thereof.
  • Optical commumcation terminal 30 includes a transmitter 40 for generating an outbound optical signal having an associated polarization.
  • Transmitter 40 may be implemented by any of a number of known coherent radiation sources with or without associated optics.
  • transmitter 40 includes a laser assembly 41, beam shaping optics 42, and an optional polarizer 43.
  • transmitter 40 generates coherent radiation at a first wavelength, such as 1550 nanometers with a first linear polarization (LP,).
  • the transmitting wavelength ⁇ ⁇ may be either ⁇ , or ⁇ 2 depending on whether terminal 30 is a type "A" or "B" terminal, respectively.
  • the first linear polarization is denoted by a dot which represents vertically polarized light, i.e. light polarized perpendicular to the plane of the figure. -11-
  • transmitter 40 may include a second laser assembly 44, associated beam shaping optics 45 and an optional polarizer 46.
  • Second laser assembly 44 includes a laser operating at a second wavelength, ⁇ 2 .
  • a beam combiner 47 directs the two beams along the same optical path 49.
  • a number of approaches are known in the existing art for accomplishing the function of the beam combiner 47.
  • a grating or a dichroic mirror may be used.
  • other options well known in the art, including a wavelength division multiplexer (WDM) or a fiber-based optical switch, are also available.
  • terminal 30 includes a receiver 48 for detecting an inbound optical signal having an associated polarization.
  • Receiver 48 includes an appropriate detector 50 and associated optics, such as a selectable bandpass filter 52, which provide the required isolation.
  • Suitable bandpass filters are available in the existing art. For widely spaced wavelengths (e.g. ⁇ , and ⁇ 2 differing by more than 15 to 20 nanometers), thin-film bandpass filters will suffice, and mechanical switching can be utilized to interchange filters having the required bandpass wavelengths.
  • ⁇ , and ⁇ 2 differing by more than 15 to 20 nanometers
  • thin-film bandpass filters will suffice, and mechanical switching can be utilized to interchange filters having the required bandpass wavelengths.
  • narrow wavelength spacing one can utilize the dielectric-coated Fabry-Perot etalon aligned perpendicular to the beam propagation direction. Since an etalon passes a periodic set of wavelengths, -12-
  • Receiver 48 preferably detects optical signals having a second linear polarization (LP 2 ) which is indicated by an arrow perpendicular to the propagation direction and represents horizontal linear polarization.
  • LP 2 second linear polarization
  • a polarization beamsplitter 54 within terrninal 30 is operable to direct optical signals having the first linear polarization (LP,) from transmitter 40 while directing optical signals having the second linear polarization (LP 2 ) to receiver 48.
  • a reconfigurable polarization changer 56 is operable to change polarization of optical signals passing therethrough.
  • polarization changer 56 is responsive to a command signal received from command processor 58 to select one of a first state in which the generated signal polarization is changed from the first linear polarization (LP,) to the first polarization (P,) (while the received signal polarization, P 2 , is simultaneously changed to the second linear polarization, LP 2 ) and at least a second state in which the generated signal polarization is changed to a second polarization (P 2 ) (where the received signal polarization, P
  • the first and second linear polarizations are orthogonal linear polarizations while the first and second polarizations (transmitted and received) are orthogonal circular polarizations.
  • the first linear polarization (LP,) may be vertically -13-
  • polarization changer 56 would change the first linear polarization (LP,) to a circular polarization (P,) such as left circular polarization (LCP).
  • LCP left circular polarization
  • received signals would be right circularly polarized (RCP) and converted to horizontal linearly polarized signals by polarization changer 56.
  • polarization changer 56 Upon receipt of a command from command processor 58, polarization changer 56 would convert the first linear polarization (LP,) to the second polarization (RCP) rather than the first polarization (LCP).
  • Reconfiguration may be coordinated by the network controller (ground station) so that communicating terminals are of the proper type.
  • autonomous control of the terminal type may be performed by processors aboard the satellite(s).
  • reconfiguration also results in changing the wavelengths associated with the transmitted and received optical signals to provide the predetermined isolation.
  • the selectable bandpass filter 52 would be adjusted to account for the interchanging of transmitted and received wavelengths.
  • Polarization changer 56 may be implemented by any of a number of known devices which may reversibly control the sense of the polarized beams.
  • a retarder such as a quarter- wave plate may be used in combination with a motor 60 to rotate the quarter- wave plate by 90° about the optical beam axis to select either the first or second polarizations. Alignment tolerances are relatively large and easy to maintain with this approach since a rotating quarter- wave plate (which has plane-parallel faces) will not impose any significant beam steering on the beams passing through it.
  • a non-mechanical approach utilizing an electro-optic crystal may be used. As is known, an electro- optic crystal driven with a DC voltage controlled by command processor 58 may be used to select the appropriate polarization state. -14-
  • Polarization changer 56 may also be implemented by an active or passive polarization rotator which rotates the output polarization by 45° but maintains linear polarization. The received beam would rotate an additional 45° as is passes back through the polarization changer (rotator) to impart a total rotation of 90° as required.
  • Polarization rotators are well known in the art and are generally made from crystalline quartz cut such that the beam propagates along the crystal optic axis (c-axis). While this alternative offers the advantage of avoiding mechanical motion, it is sensitive to the relative angular rotation along the line-of- sight or optical beam axis between two communication terminals. If the two terminals undergo any relative angular rotation about the line-of-sight, that angular rotation introduces a loss into the link.
  • the loss will be sin 2 ⁇ .
  • the quarter- wave plate implementation is insensitive to the relative angular alignment of the terminals about the line-of-sight so that there would be no loss attributable to the angular orientation.
  • the transmitted and received optical commumcation signals travel along an optical path passing through a number of optical elements common to both, including polarization beam splitter 54, polarization changer 56, fine-pointing mirror 62, telescope 64, and gimbaled steering mirror 66.
  • polarization beam splitter 54 polarization changer 56
  • fine-pointing mirror 62 fine-pointing mirror 62
  • telescope 64 telescope 64
  • gimbaled steering mirror 66 This results in reduced cost, complexity, and weight.
  • the present invention utilizes a dual-wavelength approach to achieve the desired isolation between transmitted and received signals, but uses polarization-based switching (which is essentially independent of the wavelength) to separate the two beams such that they can share common output and pointing optics. This is possible due to the fact that a single set of polarization elements will function satisfactorily over a 10 to 20 nanometer range of -15-
  • Block 80 represents transmitting optical communication signals at a first wavelength ( ⁇ ,) and first polarization (P,) and receiving optical communication signals at a second wavelength ( ⁇ 2 ) and second polarization (P 2 ).
  • the transmitted and received signals travel along an optical path within the communication terminal passing through at least one optical element common to both.
  • the first and second wavelengths are selected to provide a predetermined level of isolation between transmitted and received optical communication signals within a particular communication terminal.
  • the transmitted and received signals are separated based on the first and second polarizations but substantially independently of the first and second wavelengths. As explained above, this is accomplished using a polarization beam splitter with suitable -16-
  • Block 84 represents selectively reconfiguring the commumcation terminal by interchanging the first and second wavelengths and polarizations such that optical communication signals are transmitted at the second wavelength and second polarization and received at the first wavelength and first polarization.
  • block 80 of Figure 3 may include generating signals with a first wavelength and first linear polarization as represented by block 86.
  • the first and second linear polarizations (corresponding to the generated and detected beams) are orthogonal linear polarizations whereas the first and second polarizations (corresponding to the transmitted and received beams) are orthogonal circular polarizations.
  • the polarization is changed from the first linear polarization to a selected one of the first or second (circular) polarizations as represented by block 88.
  • the polarization of the received signal will be changed from either the first or second (circular) polarization to the second linear polarization as represented by block 90.
  • a "change" in polarization may include rotation of a linear polarization as well as changing from a linear polarization to a circular polarization.
  • references to linear and circular polarizations in the text and drawings are not intended to limit the scope of the invention but rather to improve the clarity of the description.
  • the optical communication terminal may be selectively reconfigured by interchanging the transmitting and receiving polarizations and wavelengths. Transmitting and receiving polarizations may be changed by rotating a wave plate as represented by block 94. Alternatively, this step may be performed by -17-
  • the transmitting and receiving wavelengths may be interchanged by tuning the transmitter or selecting another source within the transmitter in conjunction with selecting an appropriate bandpass filter within the receiver.

Abstract

La présente invention concerne un système et un procédé de communications optique dans l'espace. A cet effet, on utilise au moins un terminal configurable fonctionnant en longueurs d'ondes doubles de façon à conserver l'isolation entre les signaux d'émission et les signaux de réception, en relation avec des procédés de commutation de polarisation servant à séparer et d'aiguiller les signaux d'émission et les signaux de réception échangés avec les émetteurs (40) et récepteurs (48) correspondants. La commutation à base de polarisation permet un aiguillage des faisceaux indépendamment de la longueur d'ondes, ce qui vient faciliter l'échange de longueurs d'onde entre signaux en émission et signaux en réception. Un convertisseur de polarisation (56) passif ou commandé tel qu'un guide d'ondes plat ou un rotateur de polarisation permet de reconfigurer le terminal de communications (30) sans qu'il y ait besoin de repositionnement ni de calage de précision associé de l'optique d'aiguillage du faisceau (54, 62, 66).
EP99971229A 1999-10-08 1999-10-08 Terminal reconfigurable pour communications laser Withdrawn EP1135876A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US1999/023708 WO2001028137A1 (fr) 1999-10-08 1999-10-08 Terminal reconfigurable pour communications laser

Publications (1)

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EP1135876A1 true EP1135876A1 (fr) 2001-09-26

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EP99971229A Withdrawn EP1135876A1 (fr) 1999-10-08 1999-10-08 Terminal reconfigurable pour communications laser

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EP (1) EP1135876A1 (fr)
JP (1) JP2003511965A (fr)
CA (1) CA2353640A1 (fr)
WO (1) WO2001028137A1 (fr)

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US10243654B1 (en) 2018-03-30 2019-03-26 Raytheon Company Electronically steered inter-satellite optical communication system and methods
US20230087712A1 (en) * 2020-02-11 2023-03-23 Reflex Photonics Inc. Methods, devices, and architectures for inter-spacecraft optical communication
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Also Published As

Publication number Publication date
CA2353640A1 (fr) 2001-04-19
WO2001028137A1 (fr) 2001-04-19
JP2003511965A (ja) 2003-03-25

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