Transmit phase control system of synchronization burst for SDMA/TDMA satellite communication system

• US 3,995,111 A
• Filed: 02/21/1975
• Issued: 11/30/1976
• Est. Priority Date: 02/26/1974
• Status: Expired due to Term

• Current Assignee: Fujitsu Limited
• Original Assignee: Fujitsu Limited
• Inventors: Tsuji, Yoshikazu, Tada, Yoshiro
• Primary Examiner(s): Morrison, Malcolm A.
• Assistant Examiner(s): Krass, Errol A.
• Application Number:
  US05/551,676
• Time in Patent Office: 648 Days
• Field of Search: 178/69.5 R, 179/15 BS, 325/4, 325/58, 325/156, 325/157, 325/158, 343/100 ST
• US Class Current: 375/358
• CPC Class Codes: H04B 7/2048 Frame structure, synchronisation or frame acquisition in SS-TDMA systems

Abstract

A transmit phase control system of synchronization burst is disclosed for use in a SDMA/TDMA satellite communication system in which a phase error between a synchronization burst transmitted from an earth station and a synchronization window, assigned as a time slot on a satellite for returning the synchronization burst, is measured and the transmit phase of the synchronization burst is controlled based on the measured value. Phase error measurement is achieved a plurality of times in connection with the received synchronization burst of each station, and a decided phase error is derived based on the measured value obtained by the plurality of measurements. The transmit phase of the synchronization burst is then controlled in accordance with the decided phase error. Further, the phase error decision is achieved at every 1/n (n being an integer larger than 1) round trip and the present synchronization burst is transmitted with its transmit phase corrected corresponding to a value that is the sum of the phase corrected value of the n preceding phase correction instants subtracted from the decided phase error at the present instant.

Claims

1. A synchronization burst transmit phase control system for an SDMA/TDMA satellite communication system including earth stations and a satellite, said satellite produceing a synchronization window through which a synchronization burst transmitted from each earth station is returned by said satellite, and a plurality of data windows for communication between predetermined groups of earth stations and between the earth stations of each group, based on a timing signal of said satellite, wherein a round trip period is defined as the time commenced by a synchronization burst transmitted from an earth station and terminated when said same synchronization burst returns to said same earth station;

each of said earth stations comprising;

transmitting means for phase correcting each successive synchronization burst at a corresponding phase correction instant, and transmitting said phase corrected synchronization bursts to said satellite;

receiving means for receiving each synchronization burst transmitted by said transmitting means and returned from said satellite;

measuring means for measuring an error between the phase of the received synchronization burst of said earth station and that of the synchronization window, a plurality of times l during a corresponding phase control interval, and producing a measured value for each error measurement, wherein said phase control interval is defined as the time between successive phase correction instants;

deciding means for determining a decided phase error as a function of said l phase error measurements and producing a phase corrected value; and

control means for receiving said phase corrected value and controlling the transmit phase of the synchronization burst with a phase control signal at a corresponding phase correction instant.

2. A synchronization burst transmit phase control system according to claim 1, wherein said synchronization burst transmitting means comprises a reference clock signal generator, a variable frequency divider for producing a frame timing as a function of the output from said reference clock signal generator and said phase corrected value, a synchronization burst generator for producing a synchronization burst as a function of the output from said variable frequency divider, and a modulator for modulating the output from said synchronization burst generator and transmitting it to said satellite;

wherein said synchronization burst receiving means comprises a demodulator for receiving and demodulating the synchronization burst returned from said satellite and a station identification circuit for identifying the synchronization burst demodulated by said demodulator;

wherein each synchronization burst comprises 2k metric bits wherein k is a predetermined integer;

wherein said phase error measuring means comprises a 2k-bit shift register for sequentially receiving said metric bits (2k bits) of said received synchronization burst, a metric pattern generator for generating a metric pattern of said synchronization burst, 2k exclusive OR circuits for comparing the outputs from said shift register and said metric pattern generator for each corresponding bit, 2k scale-of-l counters each receiving the output from a corresponding one of said 2k exclusive OR circuits, and 2k threshold deciders each receiving the output from a corresponding one of said 2k scale-of-l counters;

wherein said phase error deciding means comprises a bit-number deciding unit for deciding the bit-number of correctly received metric bits at every reception of said synchronization burst and a phase error deciding unit for deciding the phase error based on the decided bit-number; and

wherein said synchronization burst transmit phase control means comprises means for generating a phase control signal for controlling the frequency dividing ratio of said variable frequency divider as a function of said phase corrected value.

3. A synchronization burst transmit phase control system according to claim 1, wherein said phase error deciding means includes calculating means for determining the present phase corrected value by subtracting the sum of phase correctted calues of a predetermined number of preceding phase correction instants from the decided phase error at the present phase correction instant wherein said predetermined number is greater than 1.

4. A synchronization burst transmit phase control system according to claim 2, wherein said phase error deciding means includes calculating means for determining the present phase corrected value by subtracting the sum of phase corrected values of a predetermined number of preceding phase correction instants from the decided phase error at the present phase correction instant wherein said predetermined number is greater than 1.

5. A synchronization burst transmit phase control system according to claim 4, wherein said calculating means comprises a phase corrected value memory circuit for storing the sum of phase corrected values of said predetermined number of preceding phase correction instants, a subtractor circuit for subtracting the output from said phase corrected value memory circuit from the decided phase error at said present phase correction instant, and a round trip counter for actuating said subtractor circuit at each phase correction instant.

6. A synchronization burst transmit phase control system according to claim 3, wherein said calculating means comprises a phase corrected value memory circuit for storing the sum of phase corrected values of said predetermined number of preceding phase correction instants, a subtractor circuit for subtracting the output from said phase corrected value memory circuit from the decided phase error at said present phase correction instant, and a round trip counter for actuating said subtractor circuit at each phase correction instant.