WO1999049602A1 - Systeme de diffusion numerique utilisant un systeme de radiodiffusion directe par satellite et un repeteur situe sur la terre - Google Patents

Systeme de diffusion numerique utilisant un systeme de radiodiffusion directe par satellite et un repeteur situe sur la terre Download PDF

Info

Publication number
WO1999049602A1
WO1999049602A1 PCT/US1998/014280 US9814280W WO9949602A1 WO 1999049602 A1 WO1999049602 A1 WO 1999049602A1 US 9814280 W US9814280 W US 9814280W WO 9949602 A1 WO9949602 A1 WO 9949602A1
Authority
WO
WIPO (PCT)
Prior art keywords
signal
satellite
terrestrial
broadcast
division multiplexing
Prior art date
Application number
PCT/US1998/014280
Other languages
English (en)
Inventor
S. Joseph Campanella
Original Assignee
Worldspace Management Corporation
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 Worldspace Management Corporation filed Critical Worldspace Management Corporation
Priority to KR1020007010757A priority Critical patent/KR20010042231A/ko
Priority to JP2000538457A priority patent/JP2002508623A/ja
Priority to EA200001005A priority patent/EA002604B1/ru
Priority to IL13830998A priority patent/IL138309A0/xx
Priority to APAP/P/2000/001925A priority patent/AP2000001925A0/en
Priority to EP98933306A priority patent/EP1072111A4/fr
Priority to US09/647,007 priority patent/US6944139B1/en
Priority to CA002325026A priority patent/CA2325026A1/fr
Priority to OA1200000257A priority patent/OA11532A/en
Priority to AU82979/98A priority patent/AU8297998A/en
Priority to IDW20001891A priority patent/ID27313A/id
Priority to BR9815768-0A priority patent/BR9815768A/pt
Priority to PL98343075A priority patent/PL343075A1/xx
Publication of WO1999049602A1 publication Critical patent/WO1999049602A1/fr

Links

Classifications

    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04H—BROADCAST COMMUNICATION
    • H04H40/00—Arrangements specially adapted for receiving broadcast information
    • H04H40/18—Arrangements characterised by circuits or components specially adapted for receiving
    • H04H40/27—Arrangements characterised by circuits or components specially adapted for receiving specially adapted for broadcast systems covered by groups H04H20/53 - H04H20/95
    • H04H40/90—Arrangements characterised by circuits or components specially adapted for receiving specially adapted for broadcast systems covered by groups H04H20/53 - H04H20/95 specially adapted for satellite broadcast receiving
    • 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
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04H—BROADCAST COMMUNICATION
    • H04H20/00—Arrangements for broadcast or for distribution combined with broadcast
    • H04H20/02—Arrangements for relaying broadcast information
    • H04H20/06—Arrangements for relaying broadcast information among broadcast stations
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04H—BROADCAST COMMUNICATION
    • H04H20/00—Arrangements for broadcast or for distribution combined with broadcast
    • H04H20/65—Arrangements characterised by transmission systems for broadcast
    • H04H20/71—Wireless systems
    • H04H20/74—Wireless systems of satellite networks
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04H—BROADCAST COMMUNICATION
    • H04H20/00—Arrangements for broadcast or for distribution combined with broadcast
    • H04H20/20—Arrangements for broadcast or distribution of identical information via plural systems
    • H04H20/22—Arrangements for broadcast of identical information via plural broadcast systems
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04H—BROADCAST COMMUNICATION
    • H04H2201/00—Aspects of broadcast communication
    • H04H2201/10—Aspects of broadcast communication characterised by the type of broadcast system
    • H04H2201/19—Aspects of broadcast communication characterised by the type of broadcast system digital satellite radio [DSR]

Definitions

  • a digital broadcast system uses a satellite direct radio broadcast system having different downlink options in combination with a terrestrial repeater network employing different re-broadcasting options to achieve high availability reception by mobile radios, static radios and portable radios in urban areas, suburban metropolitan areas, rural areas, including geographically open areas and geographic areas characterized by terrain having high elevations.
  • DARS digital audio radio service
  • LOS line of sight
  • Receivers in existing systems which provide digital audio radio service (DARS) have been radically affected by multipath effects which create severe degradations in signal quality, such as signal fading and inter-symbol interference (1ST). Fading effects on broadcast channels to receivers can be sensitive to frequency, particularly in an urban environment or geographic areas with high elevations where blockage of line of sight (LOS) signals from satellites is most prevalent.
  • Locations directly beneath a satellite hereinafter referred to as the sub-satellite point
  • locations that depart from the sub-satellite point inherently have decreasing elevation angles and, accordingly, an increase of the earth center angle subtended between the sub-satellite point and the reception location.
  • terrestrial re-radiation is needed to achieve suitable radio reception.
  • a digital broadcast system (DBS) which overcomes a number of disadvantages associated with existing broadcast systems and realizes a number of advantages.
  • the DBS of the present invention comprises a TDM carrier satellite delivery system for digital audio broadcasts (DAB) and other digital information which is combined with a network of terrestrial repeaters for the re-radiation of satellite downlink signals toward radio receivers.
  • the terrestrial repeaters are configured to employ multipath-tolerant modulation techniques.
  • a satellite delivery system and a terrestrial repeater operate using different carrier frequencies.
  • the terrestrial repeater employs multipath-tolerant modulation techniques.
  • a satellite delivery system and a terrestrial repeater both employ multipath-tolerant modulation techniques and can be configured to use the same or different carrier frequencies, depending on the type of waveform used.
  • the satellite delivery system preferably employs a TDM or code division multiple access (CDMA)-type waveform.
  • the terrestrial repeater preferably employs a multipath-tolerant waveform such as CDMA, Adaptive Equalized TDM (AETDM), Coherent Frequency Hopping Adaptively Equalized TDM (CFHATDM) or Multiple Carrier Modulation (MCM).
  • a single geostationary satellite transmits downlink signals which can be received by radio receivers in the LOS of the satellite signal, as well as by terrestrial repeaters.
  • Each terrestrial repeater is configured to recover the digital baseband signal from the satellite signal and modulate the signal using multicarrier modulation (MCM) for retransmission toward radio receivers.
  • Radio receivers are configured to receive both a quadrature phase shift keyed (QPSK) modulated TDM bit stream, as well as an MCM stream.
  • Radio receivers are programmed to select a broadcast channel demodulated from the TDM bit stream and the MCM bit stream, and to select the broadcast channel recovered with the least errors using a diversity combiner.
  • QPSK quadrature phase shift keyed
  • a DBS which comprises two geostationary satellites in combination with a network of terrestrial repeaters.
  • the terrestrial repeaters are configured to process satellite downlink signals to achieve the baseband satellite signal and to modulate the signal using MCM.
  • Radio receivers are configured to implement a diversity decision logic to select from among three diversity signals, including the two satellite signals and the MCM signal.
  • Each radio receiver employs maximum likelihood combining of two LOS satellite signals with switch combining between the terrestrial re-radiated signal, or MCM signal, and the output of the maximum likelihood combiner.
  • a broadcast channel may be selected from the three diversity signals by using maximum likelihood combining of all three signals, that is, early and late LOS satellite signals and the MCM signal from the terrestrial repeater.
  • FIG. 1 depicts a digital broadcast system for transmitting satellite signals and terrestrial signals in accordance with an embodiment of the present invention
  • Fig. 2 is a diagram of a digital broadcast system comprising a satellite and a terrestrial repeater in accordance with an embodiment of the present invention
  • Fig. 3 is a schematic block diagram illustrating a generation of a multicarrier modulated (MCM) signal in accordance with an embodiment of the present invention
  • Fig. 4 is a schematic block diagram depicting a radio receiver arm configured to demodulate MCM signals in accordance with an embodiment of the present invention
  • Fig. 5 is a block diagram illustrating MCM signal demodulation in accordance with an embodiment of the present invention
  • Fig. 6 is a schematic block diagram depicting a radio receiver arm configured to demodulate time division multiplexed (TDM) signals in accordance with an embodiment of the present invention
  • Fig. 7 is a block diagram illustrating QPSK TDM signal demodulation in accordance with an embodiment of the present invention
  • Figs. 8 and 9 are schematic block diagrams illustrating respective embodiments of the present invention for diversity combining in a radio receiver
  • Fig. 10 illustrates a system of combining three diversity signals using a maximum likelihood decision unit in accordance with an embodiment of the present invention
  • Fig. 11 is a schematic block diagram illustrating TDM signal demultiplexing in accordance with an embodiment of the present invention.
  • Fig. 12 illustrates a system of combining bit streams recovered at a radio receiver using a maximum likelihood decision unit on a first satellite signal and a delayed second satellite signal and then a diversity combiner for terrestrial repeater signal and the output of the maximum likelihood decision unit in accordance with an embodiment of the present invention
  • Fig. 13 illustrates an arrangement for indoor reception of a broadcast signal in accordance with an embodiment of the present invention.
  • Fig. 14 illustrates an arrangement for terrestrial repeaters along a path in accordance with an embodiment of the present invention.
  • Fig. 1 depicts a digital broadcast system (DBS) 10 comprising at least one geostationary satellite 12 for line of sight (LOS) satellite signal reception at radio receivers indicated generally at 14. Another geostationary satellite 16 at a different orbital position can be provided for time and/or spatial diversity purposes as discussed below in connection with Figs. 6 and 7.
  • the system 10 further comprises at least one terrestrial repeater 18 for retransmission of satellite signals in geographic areas 20 where LOS reception is obscured by tall buildings, hills and other obstructions.
  • the radio receiver 14 is preferably configured for dual-mode operation to receive both satellite signals and terrestrial signals and to select one of the signals as the receiver output.
  • the present invention relates to a DBS 10 for optimized static, portable and mobile radio reception.
  • the DBS 10 combines line-of-sight (LOS) reception of satellite waveforms that are optimized for satellite delivery with re-radiation of the LOS signal from the satellite 12 or 16 via one or more terrestrial repeaters 18.
  • the terrestrial repeaters 18 use other waveforms which are optimized for terrestrial delivery where blockage of the satellite LOS signal occurs.
  • LOS signal blockage caused by buildings, bridges, trees and other obstructions typically occurs in urban centers and suburban areas.
  • Waveforms particularly suitable for LOS satellite transmission are Time Division Multiplex (TDM) and Code Division Multiple Access (CDMA).
  • Multipath-tolerant waveforms particularly suitable for overcoming terrestrial multipath interference encountered in blocked urban areas are CDMA, Adaptive Equalized TDM (AETDM), Coherent Frequency Hopping Adaptively Equalized TDM (CFHATDM) and Multiple Carrier Modulation (MCM).
  • AETDM Adaptive Equalized TDM
  • CFM Multiple Carrier Modulation
  • Frequency hopping is described in U.S. Patent No. 5,283,780, to Schuchman et al, which is hereby incorporated herein by reference.
  • radio receivers 14 are provided with an equalizer (not shown).
  • AETDM a TDM bit stream is received from the satellite 12 or 16. The bit stream is converted into a new TDM bit stream into which training sequences are inserted by a process called puncturing.
  • Puncturing replaces a small fraction of the TDM data bits with the training sequences.
  • the number of bits punctured is so small that the errors thereby produced are correctable at the receiver by forward error correction.
  • the new TDM bit stream is QPSK-modulated by the repeater onto a radio frequency (RF) carrier that is transmitted at high power into the multipath environment of a central city business district, for example.
  • RF radio frequency
  • This transmitted signal is received by a receiver 14 equipped with an adaptive time domain equalizer.
  • the forward error correction available in the receiver 14 corrects both the errors introduced by the puncturing and those caused by thermal noise and receiver impairments.
  • the combination of a satellite-efficient LOS waveform and terrestrial multipath interference-tolerant waveform in a DBS system is the optimum means for achieving high availability reception by mobile radios, static radios and portable radios in urban areas, suburban areas and in rural areas.
  • an MCM signal is sent from a network of terrestrial repeaters 18 deployed to cover a blocked area with high reception availability.
  • the signaling techniques described in connection with the present invention are applicable over the electromagnetic wave frequency range from 200 to 3000 MHz to facilitate the combination of LOS satellite radiation with terrestrial re-radiation of the signal received from the satellite 12 or 16.
  • Optimal satellite waveforms permit very efficient transformation of solar power, which is collected by the solar arrays of the satellites 12 and 16 into radiated radio frequency power. These waveforms are characterized by a low peak-to-average power ratio (i.e., crest factor), thereby permitting operation of high power amplifiers that feed the satellite earth-pointing antennas at or near the maximum power output and therefore the most efficient power output.
  • a TDM waveform is particularly useful for permitting operation within a few tenths of a dB of maximum power output.
  • a CDMA waveform that uses properly selected codes allows operation at approximately 2 to 4 dB below maximum power output. Because the MCM waveform is composed of the sum of hundreds of phase modulated sinusoids, as described below with reference to Fig.
  • the MCM waveform inherently possesses a high peak-to-average ratio. Consequently, a MCM waveform encounters significantly greater amplitude and phase intermodulation distortion in the satellite's high power amplifier.
  • a MCM waveform is backed in the high power amplifier and allocated a receiver implementation impairment of at least 6 dB on the down-link budget, as compared with a quadrature phase shift keying (QPSK) TDM waveform. This translates to a 4-to-l reduction in satellite power conversion, rendering the MCM waveform an unsuitable choice for satellite LOS delivery on a DBS 10.
  • QPSK quadrature phase shift keying
  • a TDM waveform is not suitable because its reception is severely impaired by multipath effects.
  • some proposed systems which use CDMA waveforms for reinforcement repeat the same program signal using one CDMA channel code for LOS satellite delivery and another CDMA channel code for terrestrial re-radiated delivery on carriers that occupy the same frequency bandwidth. Reception is achieved by means of adaptive rake receivers.
  • These proposed CDMA systems are disadvantageous because an annulus zone occurs in which reception is not possible between the region where the reinforcement signal can be received and the region where the satellite LOS signal can be received.
  • Receivers 14 in the annulus are not able to receive the terrestrial re-radiated signal because the signal power level falls below a receiver threshold for that signal. These receivers 14 are also not able to receive the satellite LOS signal because there remains sufficient re-radiated signal to jam LOS satellite reception. Thus, these receivers 14 in the annulus must move far enough away from the zone of re-radiation to decrease the re-radiated signal power to below the threshold of jamming; otherwise, LOS satellite reception is not possible.
  • the CDMA waveform is adapted to make possible its use for simultaneous delivery via satellite LOS and via terrestrial re-radiation.
  • the CDMA channel codes are assigned for each delivery to different RF carriers.
  • the orthogonality thereby created permits the two signals (i.e., the satellite LOS signal and the terrestrial repeater signal) to be separated by RF/IF filtering in the radio receiver.
  • AETDM waveforms can be satisfactorily implemented and operated in multipath environments characterized by signal propagation delays as long as 20 microseconds ( ⁇ s). Care must be exercised to ensure that signal arrivals from distant repeaters 18 do not exceed this bound.
  • the adaptively equalized re-radiated waveform can be received by radio receivers 14 designed to use the parent non-equalized TDM waveform when the former does not exhibit severe multipath. This compatibility prevents obsolescence of direct LOS non-equalized TDM radios when the AETDM re- radiation is turned on.
  • the CFHATDM waveform can be satisfactorily implemented and operated in multipath environments characterized by delays as long as 65 ⁇ s. Care must be exercised to ensure that signal arrivals from distant repeaters 18 do not exceed this bound.
  • the waveform cannot be received by radio receivers 14 designed to use the parent non- equalized TDM waveform.
  • the MCM waveform can be satisfactorily implemented and operated in multipath environments characterized by delays as long as 65 ⁇ s.
  • the maximum delay is affected by the guard time assignment given to the waveform's periodic symbol period assignment. Care must be exercised to ensure that signal arrivals from distant repeaters 18 do not exceed this bound.
  • the waveform cannot be received by radio receivers 14 designed to use the parent non-equalized TDM waveform.
  • the CDMA waveform can be satisfactorily implemented and operated in multipath environments characterized by delays determined by the span of the time delays implemented in the rake paths at the receivers 14. Care must be exercised to ensure that all signal arrivals from distant repeaters 18, multipath reflections and different satellites do not exceed this bound.
  • the waveform cannot be received by radio receivers 14 designed to use the parent non-equalized TDM waveform.
  • the satellite signals can be transmitted from one satellite 12 or 16 or from two satellites 12 and 16.
  • Use of two geostationary satellites 12 and 16 sufficiently separated in their orbits creates diversity in the LOS elevation and azimuth angles to enhance signal reception availability.
  • time diversity achieved by repeating a satellite signal from a single satellite 12 or 16, or by transmitting a signal from two satellites 12 and 16 with the properly selected time difference further enhances the reception availability.
  • a waveform comprising multiple channel TDM with QPSK, Offset QPSK, Differential QPSK, Differentially Coded QPSK, or Minimum Shift Keyed (MSK) modulation is used for the transmission of signals from a satellite for LOS reception by a radio receiver 14.
  • Terrestrial re-radiation is preferably implemented using an MCM waveform designed to carry a TDM bit stream of a capacity of up to 3.68 Mbit/s.
  • MCM is preferably implemented which creates between 400 and 1200 multiple carriers by means of an Inverse Fast Fourier Transform as described below in connection with Fig. 3, resulting in a symbol period between 200 and 300 ⁇ s. A guard interval of between 55 to 65 microseconds is included in each symbol period.
  • the MCM waveform is designed to accommodate Doppler carrier frequency shifts among multipath components occurring simultaneously. Puncturing is preferably used to eliminate bits or pairs of bits from the TDM bit stream to reduce the rate to a value of between 70% to 80% of the 3.68 Mbit/s rate.
  • a special symbol is inserted between each of a selected number of FFT-generated symbols periods to provide a means to recover symbol period timing and carrier frequency synchronization .
  • a Viterbi soft decision trellis decoder is preferably implemented to re-establish the bits or bit pairs punctured at the repeater 18, as well as all other bits transmitted, by use of an erasure technique. In this technique, the decoder simply ignores the bits in locations known to have been punctured at the repeater 18.
  • the broadcast segment 22 preferably includes encoding of a broadcast channel into a 3.68 Megabits per second (Mbps) time division multiplex (TDM) bit stream, as indicated in block 26.
  • the TDM bit stream comprises 96 16 kilobits per second (kbps) prime rate channels and additional information for synchronization, demultiplexing, broadcast channel control and services.
  • Broadcast channel encoding preferably involves MPEG audio coding, forward error correction (FEC) and multiplexing.
  • FEC forward error correction
  • the resulting TDM bit stream is modulated using quadrature phase shift keying (QPSK) modulation, as shown in block 28, prior to transmission via a satellite uplink 30.
  • QPSK quadrature phase shift keying
  • TDM satellite delivery achieves the greatest satellite on-board payload efficiency possible in terms of the conversion of solar power to electromagnetic wave power. This is because single TDM carrier per tube operation permits each satellite traveling wave tube to operate at its saturated power output, which is its most efficient operating point.
  • the TDM carrier in a typical application is designed to deliver 96 prime bit rate increments, each bearing 16 kbit/s, to small, economical radio receivers 14 located in the beams of the satellite 12 or 16. From one to eight prime rate increments are grouped to constitute a broadcast channel.
  • a broadcast channel can be divided into a number of service channels for delivery of audio, video, data and multimedia.
  • the power density delivered to the earth by TDM carriers from satellites 12 and 16 can made very high and hence provide excellent LOS reception by radio receivers 14 in automobiles and trucks when traveling on open highways in the country side and in suburban areas.
  • LOS reception is blocked, thus inhibiting suitable operation of the receiver 14 for LOS reception.
  • Attempting to overcome these conditions by raising the satellite power is both excessively expensive and technically impractical. Accordingly, a more practical alternative is to augment the direct LOS satellite reception by adding a network of terrestrial repeaters 18.
  • Locations directly beneath the satellite 12 or 16 inherently have the highest elevation angles, while locations that depart from the sub-satellite point inherently have decreasing elevation angles and an increase of the earth center angle subtended between the sub-satellite location and the reception location.
  • Receivers 14 at locations that are near the sub-satellite point are permitted virtually unblocked LOS reception and the need for terrestrial reinforcement is minimal.
  • the LOS elevation angle to the satellite becomes less than about 85 degrees, blockage by tall buildings (i.e., > 30 m) becomes significant. Accordingly, terrestrial re-radiation for gap-filling is needed to achieve satisfactory coverage for mobile radio receivers.
  • the DBS 10 of the present invention re-radiates the LOS satellite signal from a multiplicity of terrestrial repeaters 18 which are judiciously spaced and deployed within the central part of a city, as well as in metropolitan areas and suburban areas, to achieve maximum coverage.
  • This type of deployment is a recognized art for terrestrial digital audio broadcast (DAB) and cell telephone systems, and can be extended in accordance with the present invention to terrestrial re-radiation of the TDM satellite LOS signal.
  • the deployment utilizes a mix of radiated power levels (EIRP) ranging from as little as 1 to 10 watts for short range fill-in repeaters 18 (out to 1 km radius) to as great as 100 to 10,000 watts for re-radiators or repeaters having wide area coverage (from 1 km to 10 km radius).
  • EIRP radiated power levels
  • Two preferred embodiments for a DBS 10 having a satellite-LOS/terrestrial-re- radiation configuration are described below.
  • the first embodiment involves one geostationary orbit (GSO) satellite 12 or 16 having a judiciously selected longitude along the GSO arc which operates in coordination with a network of the terrestrial repeaters 18.
  • the second embodiment involves two satellites 12 and 16 having different judiciously spaced GSO longitudes to achieve space and time diversity.
  • a DBS 10 using one GSO satellite 12 with at least one terrestrial repeater 18 is shown in Fig. 2 for illustrative purposes.
  • the LOS satellite signal is received by an antenna 32 operating in conjunction with a radio receiver 34 to demodulate and recover the digital baseband signal from the signal radiated from the satellite 12.
  • a delay block 35 delays the entire digital baseband signal by the amount of time diversity delay (if any) between transmissions from the satellites 12 and 16.
  • the digital baseband signal is supplied to a terrestrial waveform modulator 36 that generates a waveform which is judiciously designed to make possible the recovery of the digital baseband signal after the waveform has been transmitted from the terrestrial repeater 18 and received by a radio receiver 14.
  • the modulated waveform is then frequency translated to a carrier frequency and amplified, as indicated by block 38.
  • the terrestrial re-radiated waveform is specifically chosen to withstand the dynamic multipath encountered over the terrestrial path between the transmitter antenna 40 and the receiver 14. This multipath is caused by reflections and diffractions from and around obstacles such as buildings 44 and terrain and from troposphere wavebending and reflections.
  • the antenna 32 is designed to have high gain (> 10 dBi) toward the satellite 12, while achieving low gain in other directions such that the LOS signal is received with low interference and consequently very high quality (i.e. error rate ⁇ 10 .
  • the demodulator and other reception elements in the receiver 34 are those designed for the LOS radio receivers 14 used in the DBS 10 and described in the aforementioned application Serial No. 08/971,049, filed November 14, 1997.
  • the radio receivers 18 are designed to receive the 3.68 Mbit/s QPSK modulated TDM bit stream.
  • the digital baseband is preferably a 3.68 Mbit/s digital waveform TDM bit stream that carries 96 16 kbit/s prime bit rate digital channels organized into broadcast channels, and side information needed to synchronize, demultiplex and control the broadcast channels and the services they bare.
  • the terrestrial waveform modulator 36 and the waveform that it generates is designed to allow reception unimpeded by the multipath vagaries indicated at 42 of the terrestrial path as described previously.
  • Possible multipath-tolerant waveforms are adaptive equalized TDM, adaptive equalized multiple carrier frequency hoppers with adaptive equalization, Fast Fourier Transform multiple carrier modulation and CDMA with rake receivers.
  • the repeater 18 is equipped to assemble the multipath-tolerant waveform, to frequency convert the waveform to the desired re-radiator transmitter RF frequency at the selected power level via the RF translator 38, and to radiate the waveform from antenna 40.
  • the antenna 40 is preferably configured to provide omni-directional or sector directional propagation in the horizontal plane and high directive toward the horizon.
  • the net antenna gain is expected to range from 10 to 16 dBi.
  • the antenna 40 can be located on top of a building and/or on a tower at a desired height.
  • the radiated power level can range from 1 to 10,000 watts of EIRP depending on the application.
  • a particularly desirable multipath-tolerant re-radiated waveform uses multicarrier modulation (MCM).
  • MCM multicarrier modulation
  • FIG. 3 A digital stream such as the 3.68 Mbit/s TDM stream is time-domain- divided into a number of parallel paths (block 102), for example, 460 parallel paths with each parallel path carrying 8000 bits per second.
  • the bits on each of these paths are paired into 2 bit symbols with one bit identified as the I (imaginary) component and the other as the Q (Real) component of a complex number. This creates a complex symbol rate of 4000 per second.
  • Discrete Inverse Fourier Transform converter implemented using a 512 coefficient Inverse Fast Fourier Transform (IFFT) 104.
  • IFFT Inverse Fast Fourier Transform
  • the output 104 of the IFFT is a set of 460 QPSK-modulated, orthogonal sine coefficients which constitute 460 narrow band orthogonal carriers, each supporting a symbol rate of 4000 per second and consequently having a symbol period of 250 ⁇ s. No carriers appear at the output of the IFFT 104 for the coefficients that are set equal to zero.
  • the IFFT multicarrier output 104 is further processed to create a guard interval
  • Ts 1-f Ts.
  • Ts 250 ⁇ s.
  • the symbol period output of the IFFT is stored in a memory every 250 ⁇ s and then played back in 187.5 ⁇ s.
  • the first samples of the IFFT output are again played back during the 62.5 ⁇ s guard interval.
  • a symbol 106 containing a synchronization symbol is introduced periodically, as indicated by block 108. This is done to provide the means for synchronizing a sampling window of 187.5 ⁇ s duration at the receiver 14 to the center of the group of multipath arrivals every 250 ⁇ s. Also, a phase reference symbol for differential reference coding of the symbol information is also added periodically. The synchronization and phase reference symbols are preferably introduced every 20 to 100 symbol periods depending on the design requirements.
  • An additional feature of the modulation design is to puncture the TDM digital bit stream, as indicated by phantom block 110, at the input to the modulator 36 to reduce the final bandwidth of the multicarrier waveform. Puncturing means selective, sparse elimination of real data bits from the data stream applied at the input to the IFFT 104. This can be done for a fraction of the bits of the stream in anticipation that the forward error correction scheme applied at the receiver 14 will simply treat the punctured bits as errors and correct them. This has the consequence of increasing the signal to noise ratio (E /N 0 ) for a desired reception BER objective by 1 to 3 dB, depending on the fraction of bits removed by the puncturing.
  • E /N 0 signal to noise ratio
  • the design for the punctured waveform proportionately reduces the bandwidth of the multicarrier modulation. For example, if the bit rate of the TDM stream is reduced by 75% , the bandwidth will also be reduced by 75%. For the example previously given, the bit rate is reduced to 2.76 Mbit/s and the multicarrier bandwidth to 1.84 MHz. Such bandwidth compression can be necessary in applications where the available frequency spectrum would otherwise be insufficient to carry the desired capacity.
  • the terrestrial repeater described with reference to Figs. 2 and 3 is used to recover a TDM satellite downlink signal, and to demodulate and reformat the TDM signal via baseband processing into a different waveform using, for example, CDMA, AETDM, MCM or CHFATDM.
  • the DBS 10 can comprise terrestrial repeaters 18 which are co-channel or non-co- channel repeaters.
  • terrestrial repeaters 18 can be provided which are co- channel gap-fillers which merely amplify and repeat a received satellite signal on the same carrier as the satellite signal.
  • terrestrial repeaters can be provided which are non-co-channel gap-fillers which amplify and repeat a satellite signal on a different carrier frequency via frequency translation. In either case, baseband processing of the satellite signal is not performed at the repeater.
  • These types of gap-fillers can be used, for example, indoors (Fig. 10) or along a roadway (Fig. 11).
  • the multicarrier modulated RF waveform is received by the antenna 201 operating in conjunction with a low noise RF front end 202, mixer 203, local oscillator 204, first intermediate frequency (IF) 205, second mixer 206, second local oscillator 207, second IF 208 to recover the multicarrier modulated carrier.
  • a multicarrier demodulator 209 recovers the TDM digital baseband signal.
  • the received modulated signal is digitally sampled by a sampler 211, as shown in Fig. 5, at a rate equal to two of four times the bandwidth of the modulation.
  • These samples are taken during a window of 187.5 ⁇ s duration which is optimally centered on the cluster of time dispersed multipath arrivals during each symbol period once every 250 ⁇ s.
  • the samples are rate down converted by a buffer memory 212 to expand them to the 460 complex time domain samples in the original 250 ⁇ s duration window.
  • These samples are then processed by an 512 coefficient FFT 213 to recover the bits of the TDM bit stream.
  • the receiver 14 next synchronizes to the TDM masterframe frame preamble via unit 214, demultiplexes and aligns the prime rate bits via unit 215 and then recovers the bits of a selected broadcast channel via unit 216.
  • BC broadcast channel
  • a two-arm receiver 14 As depicted in Fig. 6, the MCM signal is received as described with reference to Fig. 4.
  • the QPSK modulated satellite TDM RF waveform is also received by the antenna 201 operating in conjunction with the low noise RF front end 202, a mixer 220, a local oscillator 221, a first IF 222, a second mixer 223, a second local oscillator 224, and a second IF 225, to recover the QPSK-modulated TDM carrier.
  • a QPSK TDM carrier demodulator 226 comprises a QPSK demodulator 227 which recovers the TDM digital baseband.
  • the receiver 14 next synchronizes to the TDM master-frame frame preamble 228, demultiplexes and aligns the prime rate bits 229 and then recovers the bits of a selected broadcast channel. These bits are then forward error corrected 230 using the concatenation of a soft decision Viterbi decoder 231, a de-interleaver 232, and a Reed Solomon decoder 232, to recover the broadcast channel. This recovered BC is supplied as a second input to the decision/combiner unit 240.
  • the diversity combiner 240 selects which of the two input BCs is to be submitted for further processing. It does this based on selecting that BC which is recovered with the least errors. Estimates of the error counts are available from the soft decision data supplied by the Viterbi decoders 217 and 231 or the Reed Solomon decoders 219 and 233. The decision is preferably made with a hysterisis logic which requires that several errors of difference exist before the decision is reversed. This process is needed to prevent chattering between the two BCs when the decisions are nearly equally likely. The broadcast channel selected by the diversity combiner 240 is next supplied to the appropriate source decoder 244 to recover the service(s).
  • the embodiment of the DBS 10 which uses two GSO satellites 12 and 16 with terrestrial repeater 18 is shown in Fig. 8.
  • two satellites 12 and 16 are separated by between 30 degrees to 40 degrees longitude along the GSO circle.
  • One satellite repeats a signal sent from a ground station, and the other satellite repeats the same signal sent from the same ground station but delays the signal as much as 5 to 10 seconds.
  • the use of two satellites 12 and 16 separated in space results in elevation angle diversity in the LOS paths between a radio receiver 14 on the earth and each satellite 12 and 16.
  • the time delay between the two satellite signal arrivals results in time diversity.
  • Each of these types of diversity taken alone can significantly improve the availability of the LOS signal for a moving mobile receiver 14, and the improvement in availability is further significantly enhanced by both space and time diversity.
  • This two-satellite diversity configuration operates essentially the same way as the single satellite configuration with regard to the diversity between direct LOS satellite reception and terrestrial re-radiated reception, but adds the time and space diversity provided by the two satellites.
  • the signal from the early satellite is the one re-radiated by the terrestrial repeater 18. Choice of the early signal allows any delay encountered in the signal processing at the repeater 18 or the receiver 14 to be absorbed.
  • the terrestrial re-radiation network is otherwise implemented in the same way as previously described for the single satellite configuration.
  • the receiver 14 introduces appropriate compensating delays via delay units 309 and 310 to achieve simultaneous signal reception among the three received signals and implement a diversity decision logic which selects among the three diversity signals.
  • the delay unit 309 provides a time diversity delay to the early signal to compensate for the signal propagation differential between the early and late satellites 12 and 16.
  • the delay unit 310 is preferably a vernier delay to allow fine compensation for signal alignment.
  • the radio receiver diversity logic design is shown in Fig. 8. It incorporates a maximum likelihood combiner 240 for the Early and Late LOS satellite signals with a switched combiner 307 between the terrestrial re-radiated signal and the output of the maximum likelihood combiner 240. When both signals are degraded, maximum-likelihood combining can improve the quality of reception. The improvement can be as much as 3 dB in terms of threshold E b /N 0 when both signals are equally degraded.
  • the radio receiver 14 is equipped with two receiver chains 301 and 302 that individually receive and recover the TDM signals from the early and late satellites, respectively, and selects a desired broadcast channel from each. This is done for each received signal in the same manner as previously described for LOS satellite reception in Fig. 6.
  • the broadcast channel signal derived from the early satellite is delayed by a delay unit 309 comprising a memory device to align it precisely, that is, symbol by symbol, with the symbols of the broadcast channel derived from the late satellite signal. This can be done by aligning the two broadcast channels relative to one another so as to cause coincidence of their service control header preamble correlation spikes. This coincidence is detected in a correlation comparitor unit in the delay unit 309.
  • the next step is to use the maximum likelihood combiner 240 to combine the bits of the two broadcast channels, bit-by-bit, each bit expressed in soft decision form.
  • the maximum likelihood combining coefficients are determined over 1 ms blocks of bits.
  • the output of the maximum likelihood combiner 240 is applied as one input to the switched combiner 307, with the other input coming from the terrestrial re-radiated signal receiver arm 308.
  • the choice of which input is to be passed to the output is based on selecting that BC which is recovered with the least errors.
  • one of the TDM signal receiver chains e.g., receiver chain 302 for the late satellite TDM signal
  • the switched combiner 307 selects from between the output of the maximum likelihood combiner 240 and the other satellite signal receiver arm (e.g., arm 301), as shown in Fig. 9.
  • the delay units 309 and 310 can be configured to store the entire recovered bit stream for delay purposes, which requires more buffering but simplifies combining.
  • the delay units 309 and 310 can be configured to store only a portion of the recovered TDM bit stream; however, synchronization requirements for combining become more complicated.
  • estimates of the error counts are available from the soft decision data supplied by the Viterbi decoders 217 and 231 or the Reed Solomon decoders 219 and 233.
  • the decision is made with a hysterisis logic which requires that several errors of difference exist before the decision is reversed. This process is prevents chattering between the two BCs when the decisions are nearly equally likely.
  • a simple switching logic may be used in which the switch always favors the choice of the BC having the least errors.
  • Hysterisis is used to prevent chattering.
  • the latter implementation avoids the more complex maximum likelihood combining.
  • Yet another alternative could be maximum likelihood combining of the three input BCs (e.g., from receiver arms 301, 302 and 308), as shown in Fig. 10.
  • the diversity combiner shown in Fig. 10 combines three signals. Two are received from two spatially separated satellites 12 and 16, one broadcasting an early signal and the other broadcasting a late signal. The third signal is received from a terrestrial repeater 18 which rebroadcasts the early satellite signal. These signals are received by receiver arm 301 for the early satellite 12, receiver arm 302 for the late satellite 16 and receiver arm 308 for the early signal retransmitted by the repeater 18.
  • the diversity combiner 312 combines the symbols in the three signals by maximum likelihood ratio combining. By this method, the samples of the symbol appearing at the output have the highest probability of representing the original transmitted symbol.
  • the early satellite 12 and repeater 18 signals are delayed relative to the late satellite signal by delay units 309 and 310 to realign the individual symbols of the three signals causing them to be in time coincidence.
  • Simple priori adjustment of the delay units 309 and 310 suffices to coarsely align the output of the delay units 309 and 310 to within a TDM frame of 138 ⁇ s.
  • fine alignment of the symbols to the master frame preamble (MFP) of a TDM frame is nonambiguous.
  • MFPs for each signal stream are aligned by fine tuning the delay units 309 and 310 to within a small fraction of a symbol.
  • the normalized variance ⁇ x for the signal symbols is calculated from the observed samples. These variances are calculated for the early (E), late (L) and repeater 18 or gap-filler (G) signal symbols.
  • the respective signal samples of the symbols for the early, late and gap-filler signals are then multiplexed by their variance ratios q ⁇ ⁇ , (qj " and (q G ) " , which are defined as follows:
  • the diversity combiner shown in Fig. 12 first combines signals received from two satellites 12 and 16, one broadcasting an early signal and the other broadcasting a late signal. The result of this is next combined by minimum bit error decision with reception of the early signal that has been retransmitted by a gap-filler repeater 18 located on the ground.
  • the individual signals are received by the receiver arm 301 for the early satellite, the receiver arm 302 for the late satellite and the receiver arm 308 for the early signal retransmitted by the gap-filler repeater 18.
  • the maximum likelihood ratio diversity combiner 412 combines the symbols of the early and late satellite signals in the same manner described above in connection with combiner 312 in Fig. 10 for three signals. By this method, the final symbol appearing at the output of unit 412 has the highest probability of representing the original transmitted symbol .
  • the result from unit 412 is next combined with that from the terrestrial repeater 18 by minimum BER select unit 417.
  • unit 417 there are preferably two units 250 that make FEC-decoded symbol decisions for an entire broadcast channel frame of the signals applied at their inputs.
  • One unit 250 makes its decisions on the output from maximum likelihood decision unit 412, and the other unit 250 from the signal received from the terrestrial repeater 18. These decisions also provide the number of errors made with each decision observed over the duration of a broadcast frame.
  • a BER compare unit 414 operates in conjunction with a minimum BER select unit 417 to select the symbols of that broadcast frame with the least error, as determined from inputs from Viterbi FEC units 217 and 231.
  • the early and gap-filler signals are delayed by delay units 309 and 310 to realign their individual symbols to be in symbol time coincidence with the symbols received from the late satellite.
  • the delay alignment method used here is the same as that described for the implementation of Fig. 10.
  • an indoor re- radiation system 450 is provided which is illustrated in Fig. 13. Since LOS reception of a satellite signal at a radio receiver located inside a building or other structure is generally not available, unless the radio receiver 14 is located at a window in LOS of the satellite 12 or 16, indoor reinforcement of satellite signals for more complete coverage.
  • an antenna 452 can be located externally with respect to a building so as to achieve LOS reception of satellite signals.
  • a tuned RF front-end unit
  • An interconnecting cable 456 is provided to supply the signal at the output of the tuned RF front-end unit 454 to an amplifier 458.
  • the amplifier 458 is connected to a re-radiating antenna 460 located within the building.
  • the amplifier 458 is configured to increase the power of the satellite signal to a level that, when re-radiated, by the antenna 460, is sufficient to permit satisfactory indoor reception for a radio receiver.
  • the power level radiated from the antenna 460 is sufficiently high to achieve satisfactory indoor reception at locations which are not in the LOS of the satellite, but not so high as to cause instability by signals returned by the path between the indoor antenna 460 and one or more of the receiving antennas 452.
  • high isolation i.e., on the order of 70-80 dB is preferred between the indoor antenna 466 and the outdoor antenna 452.
  • the time delay between an outdoor signal and an indoor signal in the region of combination is preferably less than a fraction of the symbol width of the signal being transmitted. For example, for a symbol width of approximately 540 nanoseconds, a time delay between 50 and 100 nanoseconds can be tolerated. The time delay is generally due to the time required for a signal to travel the path comprising the outdoor antenna 452, the cable (where signals generally travel at two-thirds the speed of light), and onward to the indoor antenna 460.
  • Another delay occurs as the signal travels from the indoor antenna 460 to the radio receiver 14 in an area covered by the indoor antenna.
  • This time delay is preferably only 20% of the symbol width, that is, not more than 100 nanoseconds for a system in which the symbol width is 540 nanoseconds.
  • a terrestrial repeater 18 The purpose of a terrestrial repeater is to repeat a signal received from the satellite into areas where the signal is otherwise blocked.
  • a multiplicity of these terrestrial repeaters 18 may be placed along a roadway or other path at a height h and separated by distances ⁇ , as shown in Fig. 14. The heights and separation distances between the terrestrial repeaters need not be equal.
  • a terrestrial repeater 18 comprises a receive antenna 462 that is pointed at the satellite 12 or 16, a receiver (not shown) that recovers the signal and amplifies it with a gain that is sufficient to drive a transmit antenna 464 such as to a power flux density in the path below which is comparative to that normally expected from the satellite.
  • the transmit antenna 464 is shielded so as to prevent the transmitted signal from reaching the terrestrial repeater receive antenna 462 at a level sufficient to create instability.
  • the transmit antenna 464 radiates its power over an aperture of length L sufficient to cause path length diversity over several wavelengths between the transmitter 464 and the vehicle's receive antenna at the carrier frequency.
  • the radio receiver 14 therein receives signals coming from more than one terrestrial repeater 18. For example, in position A, a vehicle is nearest to terrestrial repeater 18b and that terrestrial repeater's signal dominates and be responsible for reception. Signals from terrestrial repeaters 18a and 18b are low because of distance and antenna pattern and cause little interference. If the vehicle is at position B, the radio receiver 14 therein receives signals from both terrestrial repeaters 18c and 18d. Since the distances are nearly equal, and assuming that the time difference between signals radiated from terrestrial repeaters 3 and 4 is adjusted to zero, the time difference of arrival between the signals received at the vehicle are sufficiently small so as to cause constructive reinforcement. By proper choice of the distances h and d in relationship with the symbol period of the digital signal being received, this condition can be achieved.
  • the signals from two terrestrial repeaters would combine alternately in-phase and out-of-phase and phases in between. When they are in phase, the signals reinforce, and when out-of-phase the signals cancel. When signal cancellation occurs, the signal is completely lost.
  • the resulting carrier phase of the signal created by addition of the terrestrial repeater carriers rotates at a rate equal to a nearly monochromatic Doppler difference, making it difficult to recover the QPSK modulation.
  • the height h is preferably relatively small when compared to distance d so as to cause the difference in distance between the vehicle and each terrestrial repeater 18 to change by an amount sufficient to assure that the signal level from any one terrestrial repeater is attenuated by 10 dB or more compared to that from a terrestrial repeater immediately overhead.
  • the length L is preferably between 5 to 10 feet to provide sufficient path length diversity at L-band frequencies. If an equalizer unit is incorporated in the vehicle's mobile receiver 14, the time difference in arrival can be extended to several symbols, thus increasing the distance between the terrestrial repeaters to over 1000 feet. An equivalent time difference would be to transmit the signal several times from the same source over a spread not exceeding 5-10 nanoseconds. While various embodiments have been chosen to illustrate the invention, it will be understood by those skilled in the art that various changes and modifications can be made therein without departing from the scope of the invention as defined in the appended claims.

Landscapes

  • Engineering & Computer Science (AREA)
  • Signal Processing (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radio Relay Systems (AREA)
  • Mobile Radio Communication Systems (AREA)

Abstract

On décrit un système de diffusion numérique qui utilise un système de radiodiffusion directe par satellite ayant différentes options de modulation de liaison descendante qui fonctionne en association avec un réseau de répéteurs situés sur la Terre utilisant différentes options de modulation de réémission pour assurer la réception à disponibilité élevée par des radios mobiles (14), des radios statiques et des radios portatives (14) situées dans des zones urbaines, des zones de banlieue métropolitaine et dans des zones rurales, y compris dans des zones géographiquement ouvertes et dans des zones géographiques se caractérisant par des éléments montagneux élevés. On utilise des récepteurs à deux ou à trois bras qui comprennent chacun une architecture mixte permettant de recevoir les signaux provenant des satellites ou de la Terre, et de combiner avec un maximum de vraisemblance les signaux reçus pour des objectifs de diversité. Un répéteur situé sur la Terre est prévu pour reformater un signal de satellite MRT sous forme d'un signal terrestre modulé à porteuses multiples. Des configurations de répéteurs terrestres couverts ou de plein air sont également décrites.
PCT/US1998/014280 1998-03-27 1998-07-10 Systeme de diffusion numerique utilisant un systeme de radiodiffusion directe par satellite et un repeteur situe sur la terre WO1999049602A1 (fr)

Priority Applications (13)

Application Number Priority Date Filing Date Title
KR1020007010757A KR20010042231A (ko) 1998-03-27 1998-07-10 위성 직접 방송 및 지상 중계기를 이용한 디지털 방송시스템
JP2000538457A JP2002508623A (ja) 1998-03-27 1998-07-10 衛星直接放送および地上中継器を使用したデジタル放送システム
EA200001005A EA002604B1 (ru) 1998-03-27 1998-07-10 Цифровая вещательная система, использующая спутниковое прямое вещание и наземный ретранслятор
IL13830998A IL138309A0 (en) 1998-03-27 1998-07-10 Digital broadcast system using satellite direct broadcast and terrestrial repeater
APAP/P/2000/001925A AP2000001925A0 (en) 1998-03-27 1998-07-10 Digital broadcast system using satellite direct broadcast and terrestrial repeater.
EP98933306A EP1072111A4 (fr) 1998-03-27 1998-07-10 Systeme de diffusion numerique utilisant un systeme de radiodiffusion directe par satellite et un repeteur situe sur la terre
US09/647,007 US6944139B1 (en) 1998-03-27 1998-07-10 Digital broadcast system using satellite direct broadcast and terrestrial repeater
CA002325026A CA2325026A1 (fr) 1998-03-27 1998-07-10 Systeme de diffusion numerique utilisant un systeme de radiodiffusion directe par satellite et un repeteur situe sur la terre
OA1200000257A OA11532A (en) 1998-03-27 1998-07-10 Digital broadcast system using satellite direct broadcast and terrestrial repeater.
AU82979/98A AU8297998A (en) 1998-03-27 1998-07-10 Digital broadcast system using satellite direct broadcast and terrestrial repeater
IDW20001891A ID27313A (id) 1998-03-27 1998-07-10 Sistem penyiaran digital yang menggunakan siaran langsung dari satelit dan alat pemindah di bumi
BR9815768-0A BR9815768A (pt) 1998-03-27 1998-07-10 Sistema de difusão digital usando satélite diretode difusão e repetidora terrestre
PL98343075A PL343075A1 (en) 1998-03-27 1998-07-10 Digital broadcast system using satellite direct broadcast and terrestrial repeater

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US60/079,591 1998-03-27
US5866398A 1998-04-10 1998-04-10
US09/058,663 1998-04-10

Publications (1)

Publication Number Publication Date
WO1999049602A1 true WO1999049602A1 (fr) 1999-09-30

Family

ID=22018164

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US1998/014280 WO1999049602A1 (fr) 1998-03-27 1998-07-10 Systeme de diffusion numerique utilisant un systeme de radiodiffusion directe par satellite et un repeteur situe sur la terre

Country Status (3)

Country Link
SA (1) SA98190417A (fr)
WO (1) WO1999049602A1 (fr)
ZA (1) ZA983650B (fr)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1115218A2 (fr) * 1999-12-16 2001-07-11 Lucent Technologies Inc. Trame de transmission pour un système de radiodiffusion audionumérique par satellite
EP1266470A1 (fr) * 2000-02-29 2002-12-18 Worldspace Management Corporation Procede et appareil de reception et de synchronisation de plate-forme mobile dans un systeme de radiodiffusion par satellite numerique direct
WO2003041412A1 (fr) * 2001-10-18 2003-05-15 Korea Digital Satellite Broadcasting Co., Ltd. Systeme a repeteurs pour diffusion par satellite
WO2003065617A1 (fr) * 2002-02-01 2003-08-07 Alcatel Systeme et procede permettant une exploitation efficace des frequences dans un systeme de diffusion hybride a satellite a faisceaux multiples
DE102005007548A1 (de) * 2005-02-18 2006-08-24 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren und System zum optimierten Empfang von Satellitensignalen, insbesondere in Gebäuden, zur Realisierung eines globalen Warnsystems beispielsweise auf Basis eines Satellitennavigationssystems
WO2006137105A1 (fr) * 2005-06-23 2006-12-28 Finmeccanica S.P.A. Systeme de transmission par satellite ou par voie radioelectrique de signaux numeriques, protege contre les attenuations periodiques et/ou non periodiques
EP1841105A3 (fr) * 2006-03-30 2011-03-23 LG Electronics Inc. Terminal mobile et procédé pour la gestion d'informations de service de diffusion à l'aide d'une fonction de réception de diffusion numérique
US9191132B2 (en) 2009-12-28 2015-11-17 Samsung Electronics Co., Ltd. Broadcast retransmitting method, and broadcast retransmitting apparatus, broadcast output apparatus, and broadcast retransmitting system using the same

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5303393A (en) * 1990-11-06 1994-04-12 Radio Satellite Corporation Integrated radio satellite response system and method
US5319673A (en) * 1992-04-10 1994-06-07 Cd Radio Inc. Radio frequency broadcasting systems and methods using two low-cost geosynchronous satellites
US5485485A (en) * 1992-04-10 1996-01-16 Cd Radio Inc. Radio frequency broadcasting systems and methods using two low-cost geosynchronous satellites and hemispherical coverage antennas
US5659353A (en) * 1995-03-17 1997-08-19 Bell Atlantic Network Services, Inc. Television distribution system and method

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5303393A (en) * 1990-11-06 1994-04-12 Radio Satellite Corporation Integrated radio satellite response system and method
US5319673A (en) * 1992-04-10 1994-06-07 Cd Radio Inc. Radio frequency broadcasting systems and methods using two low-cost geosynchronous satellites
US5485485A (en) * 1992-04-10 1996-01-16 Cd Radio Inc. Radio frequency broadcasting systems and methods using two low-cost geosynchronous satellites and hemispherical coverage antennas
US5659353A (en) * 1995-03-17 1997-08-19 Bell Atlantic Network Services, Inc. Television distribution system and method

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP1072111A4 *

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1115218A2 (fr) * 1999-12-16 2001-07-11 Lucent Technologies Inc. Trame de transmission pour un système de radiodiffusion audionumérique par satellite
EP1115218A3 (fr) * 1999-12-16 2005-01-05 Lucent Technologies Inc. Trame de transmission pour un système de radiodiffusion audionumérique par satellite
US6956814B1 (en) * 2000-02-29 2005-10-18 Worldspace Corporation Method and apparatus for mobile platform reception and synchronization in direct digital satellite broadcast system
EP1266470A1 (fr) * 2000-02-29 2002-12-18 Worldspace Management Corporation Procede et appareil de reception et de synchronisation de plate-forme mobile dans un systeme de radiodiffusion par satellite numerique direct
EP1266470A4 (fr) * 2000-02-29 2005-01-12 Worldspace Corp Procede et appareil de reception et de synchronisation de plate-forme mobile dans un systeme de radiodiffusion par satellite numerique direct
WO2003041412A1 (fr) * 2001-10-18 2003-05-15 Korea Digital Satellite Broadcasting Co., Ltd. Systeme a repeteurs pour diffusion par satellite
WO2003065617A1 (fr) * 2002-02-01 2003-08-07 Alcatel Systeme et procede permettant une exploitation efficace des frequences dans un systeme de diffusion hybride a satellite a faisceaux multiples
US7953367B2 (en) * 2002-02-01 2011-05-31 Alcatel System and method for efficient frequency use in a hybrid multi-spot satellite broadcasting system
DE102005007548A1 (de) * 2005-02-18 2006-08-24 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren und System zum optimierten Empfang von Satellitensignalen, insbesondere in Gebäuden, zur Realisierung eines globalen Warnsystems beispielsweise auf Basis eines Satellitennavigationssystems
WO2006137105A1 (fr) * 2005-06-23 2006-12-28 Finmeccanica S.P.A. Systeme de transmission par satellite ou par voie radioelectrique de signaux numeriques, protege contre les attenuations periodiques et/ou non periodiques
EP1841105A3 (fr) * 2006-03-30 2011-03-23 LG Electronics Inc. Terminal mobile et procédé pour la gestion d'informations de service de diffusion à l'aide d'une fonction de réception de diffusion numérique
US8473985B2 (en) 2006-03-30 2013-06-25 Lg Electronics Inc. Mobile terminal and method of managing broadcasting service information using digital broadcast reception function
US9191132B2 (en) 2009-12-28 2015-11-17 Samsung Electronics Co., Ltd. Broadcast retransmitting method, and broadcast retransmitting apparatus, broadcast output apparatus, and broadcast retransmitting system using the same

Also Published As

Publication number Publication date
ZA983650B (en) 1998-11-24
SA98190417A (ar) 2005-12-03

Similar Documents

Publication Publication Date Title
US6944139B1 (en) Digital broadcast system using satellite direct broadcast and terrestrial repeater
US6956814B1 (en) Method and apparatus for mobile platform reception and synchronization in direct digital satellite broadcast system
US10110298B2 (en) Techniques for providing broadcast services on spot beam satellites
US5907582A (en) System for turbo-coded satellite digital audio broadcasting
US7646834B2 (en) Method and apparatus for combining transponders on multiple satellites into virtual channels
EP1880476B1 (fr) Procede et recepteur pour la demodulation hierarchiques de signaux radio numerique
US6452989B1 (en) System and method for combining multiple satellite channels into a virtual composite channel
EP1072111A1 (fr) Systeme de diffusion numerique utilisant un systeme de radiodiffusion directe par satellite et un repeteur situe sur la terre
EP1950894B1 (fr) Procédé de téléappel à forte pénétration
EP1705853B1 (fr) Démodulation d'information d'amplitudes dans des signaux de type OFDM modulés différentiellement
US6728202B1 (en) Code division multiplex satellite broadcasting system
WO1999049602A1 (fr) Systeme de diffusion numerique utilisant un systeme de radiodiffusion directe par satellite et un repeteur situe sur la terre
ES2311054T3 (es) Sistema y metodo para el uso eficiente de frecuencias en un sistema hibrida multihaz de radiodifusion por satelite.
EP1729473B1 (fr) Optimisation d'un réseau monofréquence par changement de la phase et de l'amplitude
De Gaudenzi et al. Analysis of an advanced satellite digital audio broadcasting system and complementary terrestrial gap-filler single frequency network
MXPA00009276A (en) Digital broadcast system using satellite direct broadcast and terrestrial repeater
CZ20003260A3 (cs) Digitální vysílací systém s přímým satelitním vysíláním a pozemním převaděčem
KR100492256B1 (ko) 위성 방송 중계기
ZA200206847B (en) Method and apparatus for mobile platform reception and synchronization in direct digital satellite broadcast system.

Legal Events

Date Code Title Description
WWE Wipo information: entry into national phase

Ref document number: 98813934.0

Country of ref document: CN

AK Designated states

Kind code of ref document: A1

Designated state(s): AL AM AT AT AU AZ BA BB BG BR BY CA CH CN CU CZ CZ DE DE DK DK EE EE ES FI FI GB GE GH GM HR HU ID IL IS JP KE KG KP KR KZ LC LK LR LS LT LU LV MD MG MK MN MW MX NO NZ PL PT RO RU SD SE SG SI SK SK SL TJ TM TR TT UA UG US UZ VN YU ZW

AL Designated countries for regional patents

Kind code of ref document: A1

Designated state(s): GH GM KE LS MW SD SZ UG ZW AM AZ BY KG KZ MD RU TJ TM AT BE CH CY DE DK ES FI FR GB GR IE IT LU MC NL PT SE BF BJ CF CG CI CM GA GN GW ML MR NE SN TD TG

121 Ep: the epo has been informed by wipo that ep was designated in this application
DFPE Request for preliminary examination filed prior to expiration of 19th month from priority date (pct application filed before 20040101)
WWE Wipo information: entry into national phase

Ref document number: PV2000-3260

Country of ref document: CZ

Ref document number: 138309

Country of ref document: IL

ENP Entry into the national phase

Ref document number: 2325026

Country of ref document: CA

Ref document number: 2325026

Country of ref document: CA

Kind code of ref document: A

WWE Wipo information: entry into national phase

Ref document number: PA/a/2000/009276

Country of ref document: MX

WWE Wipo information: entry into national phase

Ref document number: 82979/98

Country of ref document: AU

WWE Wipo information: entry into national phase

Ref document number: 1998933306

Country of ref document: EP

Ref document number: 09647007

Country of ref document: US

Ref document number: 2000/02768

Country of ref document: TR

WWE Wipo information: entry into national phase

Ref document number: 1020007010757

Country of ref document: KR

WWE Wipo information: entry into national phase

Ref document number: 200001005

Country of ref document: EA

REG Reference to national code

Ref country code: DE

Ref legal event code: 8642

WWP Wipo information: published in national office

Ref document number: 1998933306

Country of ref document: EP

WWP Wipo information: published in national office

Ref document number: PV2000-3260

Country of ref document: CZ

WWP Wipo information: published in national office

Ref document number: 1020007010757

Country of ref document: KR

WWR Wipo information: refused in national office

Ref document number: PV2000-3260

Country of ref document: CZ

WWR Wipo information: refused in national office

Ref document number: 1020007010757

Country of ref document: KR