Classifications

• • H—ELECTRICITY
  • H04—ELECTRIC COMMUNICATION TECHNIQUE
  • H04B—TRANSMISSION
  • H04B7/00—Radio transmission systems, i.e. using radiation field
  • H04B7/14—Relay systems
  • H04B7/15—Active relay systems
  • H04B7/185—Space-based or airborne stations; Stations for satellite systems
  • H04B7/18523—Satellite systems for providing broadcast service to terrestrial stations, i.e. broadcast satellite service

Definitions

• the present invention generally relates to a system for receiving a direct broadcast satellite signal from a direct broadcast satellite, and in particular, to a system for receiving direct broadcast satellite transmission in a mobile craft.
• Direct broadcast satellite systems have come into widespread use throughout the world for reception of digital television in the home, as a replacement for traditional wired cable television services.
• Direct broadcast satellite systems have also been used for high-speed Internet access, which is especially useful in areas where such access is otherwise unavailable.
• Direct broadcast satellite services have also been utilized in large recreational vehicles, airliners, and ships, where large, gimbaled dish antennas under shielding domes are employed to receive direct broadcast satellite signals.
• Such gimbaled dishes are expensive, have a large profile and are only practical in large vehicle applications in which aerodynamics are of little concern (e.g., large recreational vehicle).
• these systems rely on sizable, fast-moving antenna components and motors that have relatively high power requirements and are that typically less reliable than systems with no moving components.
• phased array antennas utilized in direct broadcast satellite systems are extremely expensive, and still have a large enough physical profile to adversely affect the aerodynamics and aesthetic appearance. Such phased array antennas also have relatively low gain in relation to their large size. Aside from size, power, and cost factors, mobile satellite reception of direct broadcast satellite signals pose several other unique challenges. These include continuous fine-tuning of the aperture, tracking during loss of signal due to obstacles (e.g., bridges, trees, etc.) or vehicle orientation (e.g., steep banking turns in small aircraft), and reliability of electronics, especially in view of poorly damped physical turbulence.
• obstacles e.g., bridges, trees, etc.
• vehicle orientation e.g., steep banking turns in small aircraft
• a mobile craft e.g., automobiles, vans, trucks, aircraft, boats, etc.
• the system of the present invention achieves one or more of these objectives by providing a system for receiving broadcast satellite transmissions.
• the system may include an orientation system for determining at least a first orientation of the vehicle or mobile craft, in three dimensions, a controller or processor in communication with the orientation system to determine first position control data, and an electronically-pointable antenna adapted to receive the first position control data from the controller to point in accordance therewith, such that a first direct broadcast satellite signal is receivable from a first direct broadcast satellite, and a direct broadcast satellite receiver adapted to process a first radio frequency signal corresponding to a first direct broadcast satellite signal received by the electronically- pointable antenna.
• the electronically-pointable antenna may be a one-dimensionally electronically-pointable antenna, and, in order to provide two-dimensional pointing, the one-dimensionally electronically-pointable antenna may be mountable upon a turntable system. Alternatively, the electronically-pointable antenna may be two- dimensionally electronically-pointable.
• the orientation system may include a solid-state electromagnetic field sensor and a fluid-filled tilt-sensor to establish absolute orientation of the system or vehicle in which the system is installed. Such orientation information, in three dimensions, may be communicated to the controller or processor to determine first position control data. Location data, for instance from a Global Positioning System receiver may also be used by the controller or processor to determine the first position control data.
• Such first position control data may include a first look-angle, which is based upon the current location and orientation of the vehicle and position of the selected direct broadcast satellite, the first look-angle being communicable to the antenna to facilitate reception thereby of a first direct broadcast satellite signal.
• the system may be an open-loop system, whereby GPS location information is received by a GPS receiver, orientation data is determined by the orientation system, and an input is receivable by a user regarding the desired direct broadcast satellite. Such data may be utilized by the controller or processor to compute a look- angle relative to the vehicle. Position control data, based upon the computed look- angle, are communicated to the electrically-pointable antenna during the absence of signal lock, as determined by the state of a signal lock detector component, or in the absence of a signal lock detector, at all times.
• the system may include a closed- looped feedback-based system, whereby the electronically-pointable antenna is continuously adjustable in one or two dimensions, and operates by receiving differential position outputs of the electronically-pointable antenna, determining adjustments to the optimal position of the antenna, and sending the adjusted position to the antenna to revise the position control data for the antenna if signal lock is present, as determined by the state of the signal lock detector.
• a closed- looped feedback-based system whereby the electronically-pointable antenna is continuously adjustable in one or two dimensions, and operates by receiving differential position outputs of the electronically-pointable antenna, determining adjustments to the optimal position of the antenna, and sending the adjusted position to the antenna to revise the position control data for the antenna if signal lock is present, as determined by the state of the signal lock detector.
• FIG. 1 is a block diagram of one embodiment of the system of the present invention.
• Fig. 2 is a schematic diagram of another embodiment of the system of the present invention.
• Fig. 3 illustrates a one-dimensionally electronically-pointable antenna mounted upon a motorized turntable.
• the system 10 includes a Global Positioning System ("GPS") receiver 20 adapted to receive GPS satellite broadcasts enabling the receiver 20 to determine the approximate location of the system 10 or craft upon which the system 10 is mounted.
• GPS Global Positioning System
• the GPS receiver 20 is flush- mounted within the roof of a vehicle in which the system 10 is installed in order to enable clearest reception of the GPS satellite broadcast signals.
• the GPS receiver 20 is in data communication with a controller or processor 40 via a serial data cable or similar device in order to enable the controller 40 to receive such information and to determine or calculate look-angles to point the antenna at the desired direct broadcast satellite.
• Such GPS receivers are commercially available from various vendors.
• this embodiment of the present invention further includes an orientation system 30 for providing orientation data to the controller or processor 40, such orientation data being usable by the controller 40 to determine look-angles to point the antenna of the system (to be described in more detail herein below) at the desired satellite.
• the orientation system 30 comprises a solid-state electromagnetic field sensor and a fluid-filled tilt-sensor adapted to measure the three-dimensional orientation of the vehicle in which the system 10 is installed.
• the solid-state electromagnetic field sensor and a fluid-filled tilt-sensor utilizes magnetometers and a fluid-filled tilt-sensor to establish absolute compass and tilt orientation of the system 10 without the use of gyroscopes.
• Such sensors perform minute measurements of the Earth's magnetic field, and use calibration software and the fluid-filled tilt sensor to overcome errors.
• This electronic compass and tilt-sensor mechanism has no moving parts other than the fluid-filled device, which does not suffer from the reliability difficulties of gyroscopes or other devices, which may require mechanical bearings. While the tilt-sensor device can be affected by lateral acceleration forces to cause inaccurate readings, the tilt- sensor device allows for accurate position tracking during any period of vehicle movement without heavy acceleration. This allows the antenna of the system 10 to be pointed accurately during most vehicle operations.
• a controller 40 may be adapted to determine the correct vehicle position by using time-differentiation of the compass orientation to determine the amount at which to compensate for tilt-sensor errors due to lateral acceleration, by methods known in the art.
• the orientation system comprising an electronic compass and tilt- sensor are available from a variety of commercial vendors, such as Precision Navigation Inc., and the three-dimensional position data may be communicated to the controller 40 via a digital or analog output, such as an EIA/TIA-232 serial link.
• the system 10 further includes the controller 40, which is adapted to receive the location data from the GPS receiver 20 and the three- dimensional orientation data from the orientation system 30.
• the controller 40 is also adapted to receive from a first user a first input corresponding to a first desired direct broadcast satellite.
• Pre-cached information or information from the GPS receiver 20 is also utilized by the controller 40 to determine true north orientation of the system 10 from the GPS location data and the magnetic position of the compass of the orientation system 30 of the present invention.
• the controller is adapted to utilize this information and to perform any coordinate conversions as necessary to compute look-angles relative to the vehicle with which the system 10 is mounted, based upon the user-selected direct broadcast satellite, current location and orientation of the vehicle.
• the controller 40 is adapted to determine position control inputs or data based upon the computed look-angle, and transmits such position control data to the antenna 50. In the event there is no closed-loop fine-tuning circuit, such position control data is transmitted to the antenna 50 continuously.
• the position control data is sent to the antenna 50 by the controller 40 during absences of signal lock, as determined by the state of a signal lock detector which controls the activation/deactivation of the closed- loop fine-tuning circuit.
• a signal lock detector which controls the activation/deactivation of the closed- loop fine-tuning circuit.
• Such signal lock detectors and closed-loop fine-tuning circuits are commercially available.
• Position control of the antenna 50 comes from the controller 40 during initial acquisition or lost signal.
• the Antenna 50 is otherwise controlled by the closed-loop fine-tuning circuit which continuously adjusts position of antenna 50.
• the controller 40 includes a personal computer, such as an Embedded Windows NT or Windows CE computer, with PCMCIA input/output cards to exchange data with the other system elements (e.g., receiver 20, orientation system 30, antenna 50).
• a personal computer such as an Embedded Windows NT or Windows CE computer
• PCMCIA input/output cards to exchange data with the other system elements (e.g., receiver 20, orientation system 30, antenna 50).
• This will allow for simple and inexpensive modifications and upgrades to the system 10. It could also provide the cost/saving benefits of a built-in television and multi-media display and web browsing capabilities to the occupants of the vehicle in which the system 10 is installed, without the need for external television monitors or web-browsing devices.
• the system 10 can be open-loop in nature in that the controller 40 can utilize data from the orientation system 30 and the GPS receiver 20 to calculate coarse look-angle for the antenna 50 in order to point it at all times.
• the controller 40 includes a signal lock detector and closed-loop feedback control circuit 70, whereby once the antenna 50 is pointed by approximation (e.g., X-Y input positions) and the expected direct broadcast signal is detected on the antenna 50 by the signal lock detector, the closed- loop fine-tuning feedback circuit begins steering the antenna 50 and input from the controller 40 will not be needed until signal is lost again. Such loss of signal may be due to obstacles or unusual vehicle orientation.
• the controller 40 is designed to steer the antenna 50 during these periods of initial signal acquisition or loss of signal.
• the antenna 50 can be steered to optimum reception during periods of satellite visibility, and held close to the optimum position during periods of occlusion, in order to minimize time to regain the best reception when the satellite becomes visible again. In these such cases, the antenna 50 acts as a "mono-pulse feed".
• the antenna 50 may be adapted to put out two or more "differential" outputs, to thereby point the antenna slightly left or slightly right, or slightly up or slightly down, depending on how the antenna 50 is configured.
• the antenna 50 may be capable of very fine directional tuning in one or both dimensions (e.g., X-Y dimensions or Azimuth and Elevation dimensions).
• the overall cost of the system 10 may be reduced by including the closed-loop fine-tuning circuit 80, so that less precise and less expensive GPS and orientation system elements may be used, and less computing power may be required of the controller 40.
• the system 10 includes an electronically-pointable antenna 50 capable of being installed on the roof of a car, truck, boat, airplane or other mobile craft with little or no adverse affect on vehicle aerodynamics.
• the antenna 50 of the system 10 of the present invention is electronically-pointable.
• the antenna 50 has a substantially flat physical profile and comprises, for example, a small phased array or plasma grating antenna capable of position scanning in two dimensions.
• Position scanning in two dimensions refers to the capability of such antennas to change their internal electronic configuration is such a way as to enable such antenna to selectively receive the signal from a particular direction, selectable along two orthogonal axes. This direction is referred to as the direction in which the antenna is "pointed", even though the antenna 50 may not physically move at all, hence the term "electronically- pointable".
• the antenna 50 comprises a phased array antenna, such as those currently available from Harris Corp. and the Boeing Corp.
• the antenna 50 comprises a scanning array available from ThermoTrex Corporation or a plasma grating antenna commercially available from WaveBand Corporation.
• the antenna 50 may be mounted on a flat motorized turntable 54 such as illustrated in Fig. 3.
• Electronic pointing in a single dimension may be continuously adjustable or discreetly adjustable.
• antennas such as an older phased array system and the antennas built by ThermoTrex Corporation, such as a scanning array can generally be adjusted to point in a continuum of positions along an axis, and these antennas can be continuously fine-tuned using a feedback loop control circuit illustrated in Fig.
• a one-dimensionally electronically-pointable antenna 50 may be mounted on a motorized turntable 54 in order to give it two-dimensional pointing capability.
• the orientation of the turntable 54 can be continuously variable and could be kept pointed at the correct relative Azimuth of the desired direct broadcast satellite with an electronic feedback loop, while the antenna 50 mounted on the turntable 54 would be adjusted for the correct relative elevation.
• the antenna 50 comprises an electronically-pointable antenna adapted to be pointed along both axes or dimensions.
• the relative Azimuth and Elevation (i.e., spherical coordinates) of the desired direct broadcast satellite can be converted in to X-Y directions (i.e., Cartesian coordinates) and the antenna 50 would be pointed along X and Y axes relative to the orientation of the vehicle in which the system antenna is mounted.
• the antenna 50 is adapted to receive position control data or look-angles from the controller 40 which dictate the direction in which the antenna 50 is to point in two-dimensions. As such, once the antenna 50 is pointed at the desired broadcast satellite, a direct broadcast satellite radios signal may enter the antenna 50. Direct broadcast radios signals may be received into the aperture of the antenna 50 and transmitted to a direct broadcast satellite receiver 60 of the system 10. This may occur after filtering and down-conversion to a lower frequency.
• the antenna 50 has a single radio frequency output, with polarization determined by a polarization input designed to select the appropriate polarization to match a particular incoming direct broadcast signal.
• a direct broadcast satellite receiver may switch the polarization of the antenna 50 between right-hand circular and left- hand circular polarization in order to change between two adjacent digital television channels on a typical direct broadcast satellite system.
• Other antennas 50 may have an independent radio frequency output for each desired signal polarization. In either case, this output is receivable by the receiver 60. This output may also be fed to a circuit controller 40 in order to determine the strength of the incoming direct broadcast signal, for determining presence or absence of a signal lock.
• the antenna 50 includes signal outputs in addition to a primary radio frequency output, which provides relative directional signal strength of the incoming signal from the direct broadcast satellite in order to track the satellite position using a closed-loop feedback control circuit 80, substantially as described herein above in relation to Fig. 2.
• the system 10 further includes a direct broadcast system receiver 60, commonly known as a set-top box or a satellite modem for data service or a functional equivalent of one or both of these.
• Such receivers 60 are available from various vendors.
• Receiver 60 may comprise, for example, one television and one data receiver, each using output from the antenna 50.
• the main input to the receiver 60 is the radio frequency output of the antenna 50.
• This input to the receiver 60 may be via a single cable with a separately selected signal polarization or multiple cables with different polarizations.
• Output from the receiver 60 is audio and video signals to a television, CRT or other audio/video electronics or a data connection (e.g., Ethernet) to a computer in the case of a satellite modem-type receiver.
• the satellite modem may be installed directly into a personal computer or similar computer.
• Either television or data from the receiver 60 can be displayed on the computer component of the controller 60, as noted herein above to save costs, or to a separate display unit.

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• Engineering & Computer Science (AREA)
• Physics & Mathematics (AREA)
• Astronomy & Astrophysics (AREA)
• Aviation & Aerospace Engineering (AREA)
• General Physics & Mathematics (AREA)
• Computer Networks & Wireless Communication (AREA)
• Signal Processing (AREA)
• Radio Relay Systems (AREA)
• Variable-Direction Aerials And Aerial Arrays (AREA)
• Circuits Of Receivers In General (AREA)
• Position Fixing By Use Of Radio Waves (AREA)
• Input Circuits Of Receivers And Coupling Of Receivers And Audio Equipment (AREA)

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Citations (5)

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• 2001
  • 2001-03-19 GB GB0218231A patent/GB2378581B/en not_active Expired - Fee Related
  • 2001-03-19 WO PCT/US2001/008700 patent/WO2001073955A2/en active Application Filing
  • 2001-03-19 CA CA002399205A patent/CA2399205C/en not_active Expired - Fee Related
  • 2001-03-19 JP JP2001571563A patent/JP2003529270A/ja active Pending
  • 2001-03-19 AU AU2001252930A patent/AU2001252930A1/en not_active Abandoned
  • 2001-03-19 DE DE10195987T patent/DE10195987T1/de not_active Withdrawn
• 2002
  • 2002-08-28 SE SE0202542A patent/SE524763C2/sv not_active IP Right Cessation

Patent Citations (5)

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