Communication satellite system having an increased power output density per unit of bandwidth

• US 5,208,829 A
• Filed: 03/26/1991
• Issued: 05/04/1993
• Est. Priority Date: 03/26/1991
• Status: Expired due to Term

• Current Assignee: Hughes Network Systems LLC (Echostar Corporation)
• Original Assignee: Hughes Aircraft Company (Rtx Corporation)
• Inventors: Rostami, Sasan, Soleimani, Mohammad
• Primary Examiner(s): Swann, Tod R.
• Application Number:
  US07/674,746
• Time in Patent Office: 770 Days
• Field of Search: 375/1, 375/103, 380/34, 455/63, 455/12, 455/13, 455/12.1, 455/13.1
• US Class Current: 375/141
• CPC Class Codes: H04B 1/707 using direct sequence modulation
• CPC Class Codes: H04B 7/216 Code division or spread-spectrum multiple access [CDMA, SSMA]
• CPC Class Codes: H04L 2027/0028 at passband only
• CPC Class Codes: H04L 2027/0057 quadrature phase
• CPC Class Codes: H04L 27/2273 associated with quadrature demodulation, e.g. Costas loop

Abstract

A satellite communication system for providing maximum power output in a spread spectrum signal transmission is disclosed. Spectral shaping is provided at a satellite transmitter to shape a spread spectrum so that over a bandwidth of interest, the spectrum has a maximally flat characteristic. By maximizing the spectrum amplitude flatness, the required power density for a bandwidth limitation imposed to prevent interference with other communication facilities is maintained. In each earth station receiving the transmission from the satellite, a filtering is provided of the demodulated baseband satellite signal such that the spectrum is restored to its original shape. The filters on the receive side may be analog, having the same amplitude function as the transmit spectrum shaping filter, but having an inverse phase response. This insures a matched filter condition at transmitter and receiver, maximizing signal transfer. A programmable demodulator is provided to select a demodulation mode. The programmable demodulator may receive microcode from a microprocessor configuring the PLA into a despreader, demodulator for spread spectrum applications or as a straight BPSK demodulator where the data signal has not been subject to spectrum spreading.

Claims

1. An earth station transmitter for transmitting a spread spectrum modulated data signal to a satellite comprising:

a source of data signals;

a spreading sequence generator for generating a spreading signal at a spreading signal chip rate f(c) synchronized with said data signals;

a multiplier for multiplying said data signals with said spreading signal to produce a spread spectrum signal having an amplitude versus frequency function defined by ##EQU5## where X is frequency;

a filter having an amplitude versus frequency characteristic defined by a 6-pole Butterworth function and by X/SIN X for filtering said spread spectrum signal to thereby produce a filtered spread spectrum signal which is amplitude normalized over at least a portion of said spread spectrum signal bandwidth; and

,

a converter for frequency upconverting said filtered spread spectrum signal for transmission to the satellite.

2. The earth station transmitter of claim 1 wherein said filter comprises a digital FIR filter.

3. The earth station transmitter of claim 1 wherein said Butterworth function has a passband ripple of less than 1 db over said portion of said signal bandwidth.

4. The earth station transmtter of claim 2, wherein said filter is a lowpass filter having a 3 db bandwidth substantially one half of the spreading signal chip rate f(c).

5. A satellite earth station receiver system for receiving a spread spectrum modulated data signal spectrum shaped to have a maximally flat Butterworth filtered characteristic comprising:

a down converter for frequency translating said modulated spread spectrum signal to an intermediate frequency signal;

a baseband signal processor for dividing said intermediate frequency signal into I and Q phase quadrature signals;

first and second filters for filtering respective of said I and Q signals, said filters having an impulse response time inverse to said Butterworth filtered characteristic; and

,

demodulator means connected to receive said I and Q signals demodulating data contained in said spread spectrum modulated data signal.

6. The satellite receiver of claim 5 wherein said demodulator means comprises:

analog to digital converter means connected to digitize each of said I and Q signals; and

,

digital circuit means connected to receive digitized data signals from said analog to digital converter means, and provide therefrom a signal proportional to the data signal.

7. The satellite receiver of claim 6 wherein said baseband signal processing means comprises:

a power divider connected to receive said intermediate frequency signal, and dividing said intermediate frequency signal into two signals;

first and second mixers connected to receive said two signals; and

,

a voltage controlled oscillator means providing first and second reference signals having a phase quadrature relationship to said first and second mixers, whereby said first and second mixers produce first and second quadrature detected signals.

8. The satellite communication system of claim 7 wherein said FIR filter has an impulse response time inverse to said analog filter impulse response.

9. The satellite receiver of claim 5 wherein said demodulator means comprises:

a programmable logic array, said array being programmable from first and second sets of configuration data to produce either a spread spectrum demodulator, or a non-spread spectrum demodulator; and

,

a microprocessor connected to said programmable logic array to supply programming data to said programmable logic array.

10. The satellite receiver of claim 7 wherein said programmable logic array supplies a control signal to said voltage controlled oscillator for maintaining said oscillator first and second reference signals in phase synchronism with said power divider signals.

11. The satellite communication system of claim 9 wherein said first and second filter means comprise first and second analog filters having an amplitude frequency response equal to said FIR filter amplitude frequency response.

12. A satellite communications system comprising:

means for producing a spread spectrum signal from a data signal with a spreading signal having a chip rate f(c) and having an amplitude of ##EQU6## where X is a frequency;

an FIR filter for producing from said spread spectrum signal a signal having a flat amplitude function over a substantial portion of said filter 3 db bandwidth which is substantially equal to one half of said spreading signal chip rate f(c);

modulation means for modulating said signal having said substantially flat amplitude function on a carrier signal; and

,

antenna means for transmitting said carrier signal to a satellite, wherein it is rebroadcast on a different carrier signal; and

,

a receiver including a down converter for producing an intermediate frequency signal from said satellite rebroadcast carrier signal;

a baseband demodulation means for removing said spread spectrum signal from said intermediate frequency signal, producing I and Q quadrature baseband signals;

first and second filter means for filtering said I and Q signals, said filter means having an amplitude frequency response substantially identical to said FIR filter response; and

,

demodulator means for removing said data signal from said I and Q signals.

13. In a satellite communications system for transmitting and receiving a spread spectrum data signal which is filtered by an FIR filter to spectrally shape said spread spectrum data signal, a receiver comprising:

a down converter for converting a carrier signal having said spread spectrum data signal modulated thereon to an intermediate frequency signal;

a baseband demodulator means for removing said spread spectrum data signal from said intermediate frequency signal, and forming I and Q quadrature signals;

first and second analog Butterworth filters for filtering said I and Q signals having an amplitude frequency response matched to said FIR filter which spectrally shapes said spread spectrum data signal; and

,

demodulation means for despreading said spread spectrum signal and producing therefrom said data signal.

14. The receiver of claim 13 wherein said demodulation means comprises:

a microprocessor system for storing first and second sets of configuration data, one set of configuration data defining a despreading demodulator, the other set of data defining a demodulator for processing a data signal which is not spread; and

,

a programmable logic array for receiving one or the other of said sets of configuration data, said logic array providing first and second demodulators for demodulating either a spread spectrum data signal or a data signal which is not spread.

15. The receiver of claim 14, wherein said demodulator processing a data signal which is not spread is a binary phase shift key demodulator.