Patent GB-1028021-A (GB)
Title: Improvements in or relating to satellite radio communication systems and apparatus therefor
Inventor: JOWETT JOHN KENNETH SAVILE
IPC: H04B7/005
Filed: 1962-01-08
Abstract: 1,028,021. Automatic phase-control systems; radio transmitting and receiving systems. POSTMASTER GENERAL. Jan. 8, 1963 [Jan. 8, 1962], No. 710/62. Headings H3A and H4L. In a satellite radio communication system the modulation band input at 1 to a transmitter TX includes the frequency of a pilot source 14 modulated by 10 c/s. and 100 c/s. oscillators 16, 17, and each of the latter is in turn compared in phase in comparators 23, 24 with the oscillations after detection by a receiver RX receiving a return of the same signal, and the comparator outputs used for adjusting a variable delay in the path of the modulation signals at both the transmitter and receiver so that the total transmission time for the modulation is maintained constant. Due to this, Doppler frequency shift errors at carrier frequency, and modulation baseband distortion, are avoided. The variable delay may be a magnetic tape or drum with record and read-out heads 2, 4 and 9, 10 in the modulation and demodulation paths respectively, the read-out heads 4, 10 being mounted on an arm 12 coarsely and finely adjustable by a motor 13 in response to outputs on phase comparators 23, 24 in turn. The pilot frequency is filtered out at 19 and, after demodulating at 20, the reference 10 c/s. and 100 c/s. tones filtered out at 21, 22. Alternatively, the 10 c/s. and 100 c/s. oscillations from 16, 17 may be added directly into the modulation or the pilot frequency may be a transmitted radio frequency. The modulation and pilot signals may be simultaneously passed to different transmitters and receivers communicating with different satellites, and each with corresponding variable delay units so that the total delay is the same in transmitting to all satellites, and programmes may be stacked in the satellites without frequency distortion. Switching in of different satellites, e.g. relaying TV programmes, is thus facilitated. The total transmission time is a multiple of the period of oscillators 16, 17 and the latter may be adjustable in frequency. The outputs of heads 2, 4 may be applied to a comparator sensing the rate of change of delay and phase difference (i.e. frequency comparator) and its output used for adjusting the transmitter frequency and/or receiver local oscillator frequency to correct the Doppler shift of carrier frequency otherwise produced at the receiver. In Fig. 4 (not shown), the transmitted pilot frequency is acted on by phase shifters to produce two versions differing in phase by 90 degrees which are applied in push-pull, together with the detected pilot frequency at the receiver, to four rectifiers feeding the four stator coils of a four-phase reluctance motor whose rotor variably adjusts the arm 12 in accordance with the rate of change of the phase difference (i.e. the frequency difference between the transmitted and received pilot frequencies due to Doppler shift) and also the phase difference. The arm 12 then adjusts the heads 4, 10 so that, by selector switches, either the transmitted or received modulation is variably delayed to maintain the modulation total transmission time and its rate of change constant and eliminate Doppler frequency shift. The transmission may be by frequency modulation, or double or single sideband amplitude modulation, or by pulse or pulse code modulation.