Patent Document

FIELD OF THE INVENTION 
       [0001]    The invention relates to minimizing an impact of noise floor variations and expanding a dynamic range on inroutes in a satellite communication system. In particular, the invention relates to minimizing an impact of noise floor variations, mainly caused by, but not limited to, self-interference effects of a satellite gateway&#39;s forward link transmissions in a Ka band spot beam satellite system, and further relates to expanding the dynamic range of the Ka band spot beam satellite system based on biasing automatic gain control estimates on each inroute according to a respective code rate of each received burst. 
       BACKGROUND 
       [0002]    Ka spot beam satellite systems and inroute links are subject to noise floor variations as a function of frequency. The variations are mainly due, but not limited to, self-interference effects caused by a satellite gateway&#39;s outroute transmissions. The inroute noise floor spectrum has pedestal and valley-like variations over a frequency range. Satellite terminals that range in areas having a relatively low noise floor may not have sufficient energy to establish a link on an inroute in areas having a relatively high noise floor. If a link can be established, errors may occur during a time interval in which a satellite terminal is adjusting its power level. 
         [0003]    Automatic gain control subsystems typically compute received power on a continuous burst-by-burst basis without any distinction as to underlying signal characteristics such as, for example, an operating code rate. Transmit power is proportional to the code rate. Consequently, averaging received power levels forces the automatic gain control subsystems to settle to an automatic gain control value proportional to a distribution of inroutes with varying code rates. When most inroutes are operating in clear sky conditions, the automatic gain control value will settle to a highest code rate power level. Centering the automatic gain control value at the highest code rate power level negatively affects inroute bursts received in a faded condition at lower code rates. As an example, if the automatic gain control value for an inroute settled to a power value associated with a code rate of 9/10, a burst received at a code rate of 1/2 would experience packet loss and degradation due to a limited dynamic range of a demodulator. 
       SUMMARY 
       [0004]    This Summary is provided to introduce a selection of concepts in a simplified form that is further described below in the Detailed Description. This Summary is not intended to identify key features or essential features of the claimed subject matter, nor is it intended to be used to limit the scope of the claimed subject matter. 
         [0005]    In a first aspect of the invention, a machine-implemented method is provided for minimizing the impact of noise floor variations in a Ka band spot beam satellite system. A channelizer of a satellite gateway demodulator may receive digitized signals for multiple channels. For each of the received digital signals, a respective automatic gain control component adjusts the received power level of a respective digitized signal to produce a respective automatic gain controlled digitized signal. The respective automatic gain control component is associated with a respective channel on which a corresponding analog signal was received. The respective automatic gain controlled digital signal may be downconverted to produce a respective downconverted signal. The respective downconverted signal may then be provided to a burst processor component of the demodulator. The burst processor component may determine an automatic gain control estimate for the respective downconverted signal, and may provide the automatic gain control estimate and channel information of the respective channel to a processor component, which determines an average automatic gain control value for the respective channel, based on the automatic gain control estimates for the respective channel, and provides the average automatic gain control value to the respective automatic gain control component of the channelizer within the satellite gateway. 
         [0006]    In a second aspect of the invention, a machine-implemented method for expanding the dynamic range in a Ka band spot beam satellite system is provided. Multiple digitized signals for multiple inroutes may be received by at least one automatic gain control component of a satellite gateway demodulator. For each of the received digitized signals, automatic gain control is performed, by the at least one automatic gain control component, on a respective digitized signal to produce a respective automatic gain controlled digitized signal. The respective automatic gain controlled digitized signal may be downconverted to produce a respective downconverted signal. The respective downconverted signal may be provided to a burst processor component of the demodulator. The burst processor component may determine an automatic gain control estimate for the respective downconverted signal, may obtain a code rate associated with the respective downconverted signal, and may provide the code rate and the automatic gain control estimate associated with the respective downconverted signal to a processor component of the satellite gateway. The processor component may calculate average automatic gain control values based on the determined automatic gain control estimates and a non-zero fixed bias associated with the corresponding code rate in order to maximize the demodulator dynamic range, and may provide at least one automatic gain control reference to the at least one automatic gain control component to affect the automatic gain control performed by the at least one automatic gain control component. The at least one automatic gain control reference is based on the average automatic gain control value associated with multiple downconverted signals. 
         [0007]    In a third aspect of the invention, a method is provided for a satellite terminal served by a satellite gateway that periodically advertises automatically generated noise floor information of multiple channels. The satellite terminal may periodically receive the advertised automatically generated noise floor information from the satellite gateway. The satellite terminal may periodically transmit data to the satellite gateway, an amount of power used by the satellite terminal transmitting the data is based on a latest of the periodically received advertised automatically generated noise floor information. 
         [0008]    In a fourth aspect of the invention, a satellite gateway is provided. The satellite gateway may include a processor component, a burst processor, and a channelizer for receiving digitized signals. The channelizer may include multiple channelizer automatic gain control components, multiple down converters, and a multiplexer. Each of the multiple channelizer automatic gain control components may adjust the received power level of digitized signals associated with a respective channel in order to produce a respective automatic gain controlled digitized signal. Each of the multiple down converters may be connected to a respective channelizer automatic gain control component and may be arranged to downconvert the respective automatic gain controlled digitized signal to produce a respective downconverted digitized signal. A multiplexer may be arranged to receive each of the respective downconverted digitized signals and may provide each of the respective downconverted signals to the burst processor component. The burst processor component includes a demodulator automatic gain control estimator, a demodulator automatic gain control component, and a carrier recovery loop component. The demodulator automatic gain control estimator may receive each of the respective downconverted signals, one at a time, and may produce a corresponding demodulator automatic gain control estimate. The demodulator carrier recovery loop component may receive the respective automatic gain controlled downconverted signal from the demodulator automatic gain control component and may produce respective demodulated data and respective burst information. The processor component may receive the corresponding demodulator automatic gain control estimates from the demodulator automatic gain control estimator, the demodulated data and the burst information from the demodulator carrier recovery component, and may periodically provide automatic gain control reference values to respective channelizer automatic gain control components. Each of the automatic gain control reference values are related to the automatic gain control estimates for a respective inroute. 
     
    
     
       DRAWINGS 
         [0009]    In order to describe the manner in which the above-recited and other advantages and features can be obtained, a more particular description is provided below and will be rendered by reference to specific embodiments thereof which are illustrated in the appended drawings. Understanding that these drawings depict only typical embodiments and are not therefore to be considered to be limiting of its scope, implementations will be described and explained with additional specificity and detail through the use of the accompanying drawings. 
           [0010]      FIG. 1  illustrates an exemplary noise floor in a Ka band spot beam satellite system. 
           [0011]      FIG. 2  shows an effect of interference caused by outroute transmissions in a Ka band spot beam satellite system. 
           [0012]      FIG. 3  shows a portion of a processor component and a demodulator, which includes a channelizer and a burst processor, in an existing system. 
           [0013]      FIG. 4  shows a portion of a processor component and a demodulator, which includes a channelizer and a burst processor, in an exemplary satellite gateway consistent with embodiments of the invention. 
           [0014]      FIG. 5  illustrates an exemplary process that may be performed in various embodiments of a burst processor. 
           [0015]      FIG. 6  illustrates an exemplary process performed by a channelizer consistent with embodiments of the invention. 
           [0016]      FIG. 7  is a flowchart for explaining an exemplary process that may be performed in an embodiment of a processor component. 
           [0017]      FIG. 8  illustrates a dynamic range plot of an exemplary satellite gateway demodulator. 
           [0018]      FIG. 9  illustrates an exemplary process that may be performed by a second embodiment of a processor component. 
           [0019]      FIG. 10  illustrates the automatic gain control converging to a power level when a majority of bursts are received during a clear sky condition, at a high code rate. 
           [0020]      FIG. 11  shows that, when code rate is taken into account in the second embodiment of the processor component, the automatic gain control will converge to a power level corresponding to a midpoint of all received bursts, independent of code rate. 
       
    
    
     DETAILED DESCRIPTION 
       [0021]    Embodiments are discussed in detail below. While specific implementations are discussed, it should be understood that this is done for illustration purposes only. A person skilled in the relevant art will recognize that other components and configurations may be used without parting from the spirit and scope of the subject matter of this disclosure. 
       Noise and Interference 
       [0022]    Inroute links in a Ka band spot beam satellite system are subject to noise variation as a function of frequency.  FIG. 1  illustrates an exemplary noise floor in a Ka band spot beam satellite system. An abscissa, or horizontal coordinate, represents received inroute signals at various frequencies and an ordinate, or vertical coordinate, represents a corresponding amount of power received at a satellite gateway at each inroute frequency. A thermal noise floor N 0    102  is generally flat. Signals  104 ,  106 ,  108 ,  110  represent various amounts of power used to maintain the desired satellite link performance. In general, with a flat thermal noise profile and a fixed rain fade attenuation value, the received power required varies only due to the transmission symbol rate and FEC rate, and does not vary with inroute frequency. 
         [0023]      FIG. 2 , which has a same abscissa and a same ordinate as in  FIG. 1 , shows a typical Ka band spot beam satellite system noise floor  202  due to self-interference. As can be seen in  FIG. 2 , noise floor  202  is not flat, and signals  204 ,  206 ,  208 ,  210  are received at varying noise floor levels. 
       Prior Art Demodulator and Processor Component 
       [0024]      FIG. 3  illustrates a portion of a demodulator  302  and a processor component  304  of an existing satellite gateway. Demodulator  302  may include a channelizer  306  and a burst processor  308 , as well as a radio frequency/intermediate frequency automatic gain control component (RF/IF AGC)  310  and an analog-to-digital (A/D) converter  312 . A received radio frequency or intermediate frequency analog signal may be provided to demodulator  302 . RF/IF AGC component  310  may perform automatic gain control on the received analog signal to produce an automatic gain controlled signal, which may be provided to A/D converter  312  to produce a digitized signal. The digitized signal may then be provided to channelizer  306 . 
         [0025]    Channelizer  306  may include a radio frequency or intermediate frequency automatic gain control estimator (RF/IF AGC estimator)  314 , a common channel automatic gain control (AGC) component  316 , down converter components  1  through N, where N is a number of channels or inroutes, and a multiplexer  320 . 
         [0026]    RF/IF AGC estimator  314  and common channel AGC  316  both may receive the digitized signal from A/D converter  312 . RF/IF AGC estimator  314  may estimate a value of automatic gain control from the received digitized signal and may provide the estimated value to RF/IF AGC component  310  as an automatic gain control (AGC) reference. Common channel AGC component  316  may perform automatic gain control on the received digitized signal to produce an automatic gain controlled digitized signal, which may be provided to one of down converters  1  through N ( 318 -A to  318 -N) based on an inroute on which the corresponding analog signal was received. Processor component  304  may provide an AGC reference to common channel AGC component  316 , as will be discussed later. 
         [0027]    Each of down converters  1  through N ( 318 -A to  318 -N) may receive a respective automatic gain controlled digital signal from common channelizer AGC component  316  and may downconvert the respective automatic gain controlled digital signal to produce a respective downconverted signal, which may be provided to multiplexer  320 . Multiplexer  320  may then provide the respective downconverted signals to burst processor  308 . 
         [0028]    Burst processor  308  may include a demodulator AGC estimator component  322 , a demodulator AGC component  324 , and a carrier recovery loop (CRL) component  326 . 
         [0029]    Demodulator AGC estimator component  322  and demodulator AGC component  324  may receive each respective downconverted signal from multiplexer  320 . Demodulator AGC estimator component  322  may estimate an AGC value based on the received respective downconverted signal, may provide the estimated AGC value to processor component  304  and may provide the estimated AGC value to demodulator AGC component  324  as an AGC reference for demodulator AGC component  324 . 
         [0030]      FIG. 5  illustrates an exemplary process performed by burst processor  308  in various embodiments. First, burst processor  308  receives a respective downconverted signal (act  502 ). Demodulator AGC component  324  may perform automatic gain control on the received respective downconverted signal and may produce and provide a respective downconverted automatic gain controlled signal to CRL component  326  (act  510 ). CRL component  326  may recover demodulated data and additional descriptive burst information in a form of a data header packet from the respective downconverted automatic gain controlled signal (act  512 ) and may provide the demodulated data and the burst information to processor component  304  (act  520 ). The burst information may include an inroute number, as well as other information including, but not limited to a code rate. 
         [0031]    Demodulator AGC estimator component  322  may estimate an AGC value from the received downconverted signal (act  504 ) and may provide the estimated AGC value to demodulator AGC component  324  to use as an AGC reference value (act  506 ). Demodulator AGC estimator component  322  may further provide the estimated AGC value to processor component  304  (act  508 ). 
         [0032]    Processor component  304  may include a processor for executing instructions stored in a memory, which may include volatile memory and/or non-volatile memory. When processor  304  executes the instructions, a method may be performed. 
         [0033]    Processor component  304  may receive and store, for each burst, the received AGC estimated value from demodulator AGC estimator component  322 , and the demodulated data including the burst information from CRL component  326 . Processor component  304  may calculate an average received AGC value from the AGC estimated values received during a predetermined time period. The average received AGC value may be provided by processor component  304  to common channelizer AGC component  316  as an AGC reference value. The average received AGC value may be calculated by processor component  304  based on bursts received across all inroutes and all code rates. Processor component  304  may provide an updated average received AGC value to common channelizer AGC component  316  as an updated AGC reference value. 
       Exemplary Demodulator and Processor Component Consistent with Embodiments of the Invention 
       [0034]      FIG. 4  illustrates a portion of a demodulator  402  and a processor component  404  of an exemplary satellite gateway consistent with embodiments of the invention. Reference numerals identical to those of  FIG. 3  indicate identical components and will not be further discussed. 
         [0035]    Demodulator  402  may include a channelizer  406  and burst processor  308 , as well as radio frequency/intermediate frequency automatic gain control component (RF/IF AGC)  310  and analog-to-digital (A/D) converter  312 . 
         [0036]    Channelizer  406  may include radio frequency or intermediate frequency automatic gain control estimator (RF/IF AGC estimator)  314 , channelizer automatic gain control (AGC) components  1  to N ( 416 - 1  through  416 -N) and down converter components  1  to N ( 318 - 1  through  318 -N), where N is a number of channels or inroutes, and multiplexer  320 . 
         [0037]    Each of channelizer AGC components  1  to N ( 416 - 1  through  416 -N) corresponds to a respective inroute and may perform automatic gain control on a digitized signal associated with the respective inroute to produce a respective automatic gain controlled digitized signal, which may be provided to a respective down converter of down converters  1  to N ( 318 - 1  through  318 -N) based on an inroute on which the signal was received. Processor component  404  may provide AGC references to respective channelizer AGC components ( 416 - 1  through  416 -N), as will be discussed later. 
         [0038]      FIG. 6  illustrates an exemplary process, performed by channelizer  406  when receiving a digitized signal. The process may begin with channelizer  406  receiving the digitized signal (act  602 ). A channelizer AGC component, of channelizer AGC components  1  to N ( 318 - 1  through  318 -N), associated with an inroute on which an analog signal, corresponding to the received digitized signal was received, performs automatic gain control to produce an automatic gain controlled signal (act  604 ). Next, one of down converters  1 -N ( 318 - 1  through  318 -N), associated with the channelizer AGC component, receives the automatic gain controlled signal and downconverts the automatic gain control signal to produce a downconverted signal (act  606 ). The downconverted signal may then be provided to burst processor  308  via multiplexer  320  (act  608 ). 
         [0039]    Processor component  404  may include a processor for executing instructions stored in a memory, which may include volatile memory and/or non-volatile memory. When processor  404  executes the instructions, a method may be performed. In other embodiments, processor component  404  may include an application specific integrated circuit (ASIC) or a field programmable gate array (FPGA). 
         [0040]    Processor component  404  may receive and store, for each burst, the received AGC estimated value from demodulator AGC estimator component  322 , the demodulated data and the burst information including, but not limited to, inroute number and code rate, from CRL component  326 . 
         [0041]      FIG. 7  illustrates an exemplary process that may be performed by processor component  404 . Processor component  404  may calculate an average AGC value for each inroute based on the AGC estimated values received. Processor component  404  may begin with inroute  1  (act  704 ), may determine an average AGC value based on the demodulator AGC estimates for the inroute (act  706 ), and may save the average AGC value (act  708 ). If processor component  404  has not processed a last inroute (act  710 ) then processor component  404  may increment an inroute number to prepare to process a next inroute (act  712 ). Processor component  404  may then repeat acts  706 - 708 . If, during act  710 , processor component  404  determines that average AGC values for all inroutes have been calculated, then processor component  404  may provide the average AGC values for all inroutes to respective channelizer AGC components ( 416 - 1  through  416 -N) as AGC reference values (act  714 ). Processor component  404  may then provide the AGC reference values as a noise floor map to satellite terminals served by the satellite gateway (act  716 ). The process may then be completed. 
         [0042]    As illustrated by the exemplary process of  FIG. 7 , the average received AGC estimate value for each inroute may be calculated by processor component  404  and may be provided to the respective channelizer AGC component ( 416 - 1  through  416 -N) as the respective AGC reference value. Processor component  404  may calculate the respective average AGC estimate value based on bursts received for each respective inroute regardless of code rates. Processor component  404  may provide updated average AGC estimate values to respective channelizer AGC components ( 416 - 1  through  416 -N) as AGC reference values are updated. 
         [0043]    Differences among AGC reference values for different inroutes provide an indication of noise floor variation and position. Processor component  404  may advertise a noise floor map to satellite terminals served by the satellite gateway based on the differences among the AGC reference values for different inroutes. The advertised noise floor map may be sent to the satellite terminals periodically. The satellite terminals, served by the satellite gateway, may receive and store the noise floor map and when each satellite terminal transmits, only an amount of power required for a particular code rate operating point is used, taking the noise floor map into consideration. 
       Second Processor Component Embodiment 
       [0044]    A demodulator has a finite burst-to-burst dynamic range.  FIG. 8  illustrates an exemplary demodulator&#39;s dynamic range. AGC range is represented along an abscissa of  FIG. 8  and the demodulator&#39;s probability of error performance, P(error), is represented along an ordinate of  FIG. 8 . As  FIG. 8  shows, the dynamic range of the exemplary demodulator is from −9 dB to +9 dB before demodulator error rates grow excessively. 
         [0045]    In a second embodiment of a processor component, a processor component  404 ′ may receive and store, for each burst, the received AGC estimated value from demodulator AGC estimator component  322 , and the demodulated data including burst header information from CRL component  326 . 
         [0046]      FIG. 9  illustrates an exemplary process that may be performed by processor component  404 ′. The process may begin with inroute  1  (act  904 ). Processor component  404 ′ may calculate an AGC value for each burst received on an inroute based on a difference between each respective AGC estimated value received and a respective fixed non-zero bias value associated with a corresponding burst code rate (act  906 ). The processor component may then calculate the average AGC value for the inroute by averaging the calculated AGC values for bursts received on the inroute and saving the averaged AGC value for the inroute (act  910 ). In one exemplary embodiment the fixed non-zero bias value for code rates 1/2, 2/3, 4/5, and 9/10, respectively, may be −2.5 dB, −1.25 dB, +1.25 dB, and +2.5 dB. In other embodiments, different biases may be used for different or additional code rates. 
         [0047]    Processor component  404 ′ may then determine whether a last inroute was processed (act  912 ). If the last inroute was not processed, then an inroute number is incremented to prepare to process a next inroute (act  914 ) and acts  906 - 914  may be repeated. 
         [0048]    If, during act  912 , processor component  404 ′ determines that the last inroute was processed, then processor component  404 ′ may provide the saved average calculated AGC value for each inroute to a respective channelizer AGC component ( 416 - 1  through  416 -N) as respective AGC reference values (act  916 ). Processor component  404 ′ may then send noise floor mapping information, based on the respective AGC reference values, to satellite terminals served by the satellite gateway (act  918 ). The respective average calculated AGC estimate values may be calculated by processor component  404 ′ based on bursts received for each respective inroute. After performing act  918 , the process may be completed. 
         [0049]    Differences among AGC reference values for different inroutes provide an indication of noise floor variation and position. As previously mentioned, processor component  404 ′ may advertise a noise floor map to satellite terminals served by the satellite gateway based on the differences among the AGC reference values for different inroutes. The advertised noise floor map may be sent to the satellite terminals periodically. The satellite terminals may transmit at only an amount of power required for a particular code rate operating point. 
         [0050]    If a majority of received bursts are received during a clear sky condition at a code rate of 9/10, automatic gain control will converge to a higher level than if the majority of the bursts are at a lower code rate such as, for example, 1/2. This is shown in  FIG. 10  in which the majority of the received bursts have a code rate of 9/10. As shown, bursts received with the code rate of 9/10 are centered to be in a middle of the dynamic range. 
         [0051]    When the code rate is taken into account, as it is in processor component  404 ′, automatic gain control will converge such that a middle code rate may be in an approximate central portion of the dynamic range, as shown in  FIG. 11 . 
       CONCLUSION 
       [0052]    Various embodiments have been described in this specification. Different combinations of the various embodiments are also included within the scope of this disclosure. For example, channelizer  406  may be implemented with either processor component  404 , with no code rate biasing of AGC values, or processor component  404 ′, with code rate biasing of AGC values. 
         [0053]    Although the subject matter has been described in language specific to structural features and/or methodological acts, it is to be understood that the subject matter in the appended claims is not necessarily limited to the specific features or acts described above. Rather, the specific features and acts described above are disclosed as example forms for implementing the claims. 
         [0054]    Although the above descriptions may contain specific details, they should not be construed as limiting the claims in any way. Other configurations of the described embodiments are part of the scope of this disclosure. Further, implementations consistent with the subject matter of this disclosure may have more or fewer acts than as described, or may implement acts in a different order than as shown. Accordingly, the appended claims and their legal equivalents should only define the invention, rather than any specific examples given.

Technology Category: h