The invention relates to a digital radiocommunication method and system. In particular, the invention is applicable to satellite radiocommunication systems onboard mobile ground stations capable of communicating while in movement.
A satellite connection between two ground stations must firstly satisfy user needs in terms of speed and robustness, and also a number of regulation coordination constraints. These constraints are intended particularly to limit interference between different communication systems.
For fixed or slightly mobile ground stations, the problem at the moment is solved by the use of large antennas, for example antennas with a diameter of more than 1 meter. These antennas can increase the sensitivity in reception while offering a high spatial resolution. However, the use of these large antennas is sometimes a problem for mobile ground stations capable of communicating in movement, for example such as stations onboard vehicles.
A proportion of deployed mobile ground stations is provided with conventional modems that do not manage spectrum spreading and have a small diameter antenna, for example less than 1 meter. These stations cannot set up medium and high-speed data connections and also respect regulation coordination constraints. Furthermore, these stations are sensitive to the Doppler effect, consequently limiting their use to fixed configurations during communication phases.
In particular, the purpose of the invention is to overcome the above-mentioned disadvantages. To achieve this, the purpose of the invention is a digital radiocommunication system comprising an antenna, one or several modems and frequency translators. Furthermore, the system comprises at least one device external to the modems connected firstly to at least one modem, and secondly to at least one frequency translator. This device is designed to execute mathematical processing in base band on communication signals output from the modem and/or the translator, for example such as:
This device may comprise:
The device may also comprise:
In particular, the digital radiocommunication system may belong to the ground segment of a system using satellites to relay communication signals. It can set up and maintain communications while in movement. The radiocommunication system may be conditioned:
Another purpose of the invention is a signal processing method for a digital radiocommunication transceiver used in the digital radiocommunication system.
In particular, the advantage of the invention is that it can provide a spectrum spreading modulation capacity for stations without this capability, without changing modems. Therefore, it is an economic solution. Furthermore, the invention is extendable and configurable, so that it can easily be integrated into an architecture including pendular stations, concentrators and a management segment.
Other characteristics and advantages of the invention will become clear after reading the description below with reference to the appended figures, wherein:
Compared with the system in
The emission part may for example comprise:
The processing unit 62 for signals to be emitted receives a signal in base band SE(t) obtained by multiplying the signal received from the input 51 and the signal output by the oscillator 65, this operation being done by the multiplier 61. The signal obtained at the output from the processing unit 62 for signals to be emitted is present on the output 54 after having been transposed into an intermediate frequency IF signal by multiplication (67) by the signal output by the oscillator 65.
For example, the reception part comprises:
The received signal processing unit 63 receives a base band signal SR(t) obtained by multiplying the signal received from the input 55 and the signal output by the oscillator 64, this operation being done by a multiplier 68. The signal obtained at the output from the processing unit 63 for signals to be emitted is present on the output 53, after having been transposed into a frequency signal IF by multiplication 69 by the signal output by the oscillator 65.
In particular, the programming and configuration signals include information about the frequency set value of signals in emission and in reception. They are received on the input 52 to which the control unit 66 is connected. For example, these signals may be obtained from an input on a keyboard, from an external programming device or from a control bus for modems 2. The control unit slaves the reception signals oscillator 64 and the emission signals oscillator 65 to the frequencies thus received.
For example, the processing unit 62 for signals to be emitted comprises an adder 621, a pilot time generator 622, an input 623 receiving a set spreading frequency signal F0, a pseudo-random code generator 624 generating a spreading sequence, and a multiplier 625.
A periodic signal called a pilot time signal for signals to be emitted STPE(t), the frequency of which is chosen outside the useful spectrum of the input signal, is created by the pilot time generator 622, and then added to the signal SE(t) by the adder 621. The power of this periodic signal may be limited so as to maximise the emitted useful signal power, and may for example be less than 10 dB at the useful signal power.
The resulting composite signal is then multiplied at the multiplier 625 by values output from the spreading sequence so as to produce a signal for which the spectrum is for example spread on a frequency band varying by +/−F0. The values derived from the spreading sequence are generated at the rate of the spreading frequency signal FO received from the input 623. This operation spreads the composite signal spectrum on a frequency band varying by +/−F0.
The pilot time signal of signals to be emitted STPE(t) may be a sinusoidal signal, or any other periodic signal.
The generator 623 generates a periodic signal STPR(t) called the pilot time signal of the received signals. The frequency of this signal may for example be equal to the frequency of the emissions pilot time signal. The signal SR(t) received by the received signals processing unit 63, including the emissions pilot time signal STPE(t), is multiplied by the generated periodic signal STPR(t) transmitted to the correlator 634. The correlator outputs pulses when the signal STPE(t) included in the signal SR(t) and the pilot time signal STPR(t) are in phase.
The Doppler corrector 632 then uses the phase of these pulses to generate a Doppler frequency error. This error signal is subtracted by a multiplier 631 from the signal received by the received signals processing unit 63.
The oscillator 636 pilots the frequency at which the pseudo-random code generator 637 presents a new code on its output, and is slaved by the pilot time synchronisation 635 to the position in time of pulses output from the correlator 634. The code sequence thus obtained is multiplied by the corrected Doppler error signal. The resultant signal is presented at the output from the processing unit. This signal is identical to transmission errors and, except the noise on the transmission channel, to the signal received from the input 51, in other words to the signal received from the modem 2 before processings done by the processing unit 62 for signals to be emitted.
Number | Date | Country | Kind |
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0413837 | Dec 2004 | FR | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/EP05/55387 | 10/19/2005 | WO | 00 | 4/29/2008 |