Satellite positioning apparatus
First Claim
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1. An apparatus for processing data, sent from a satellite in the form of a fixed frequency signal containing phase modulated pulse doublets or orbit definition data, to determine a position of a vehicle on the earth, comprising:
- a. receiver means for receiving the signal from the satellite, said receiver means comprising;
1. intermediate frequency means for domodulating the fixed frequency signal for processing;
2. phase detector means for determining the phase of the demodulated signal from said intermediate frequency means;
3. phase lock loop means receiving an output of said phase detector means for regulating the frequency of said intermediate frequency means;
4. doppler demodulator means responsive to an output of said phase lock loop means for determining the doppler shift in frequency of the signal sent from the satellite;
5. local oscillator means for forming a reference frequency signal;
6. synthesizer means for forming demodulating frequency signals for said intermediate frequency means, said phase detector means, and said doppler demodulator means from said reference frequency signal;
7. bit phase detector means for determining the phase of the orbit definition data phase doublets;
8. bit rate phase lock loop means for contrOlling the phase of the orbit definition data pulse doublets; and
9. data decoder means for decoding the orbit definition data from the phase modulated pulse doublets;
b. computer means for processing the doppler shift and orbit definition data to determine the location of the vehicle;
c. interface circuit means for providing the doppler shift and orbit definition data to said computer means, said interface circuit means including doppler counter means for counting the doppler shift; and
d. display means for indicating the location of the vehicle determined by said computer means.
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Abstract
A new and improved apparatus for determining the position of a vehicle or vessel on the earth'"'"''"'"'s surface by processing signals sent from a satellite, based on the doppler shift in frequency of the signals so sent, and the orbit description data encoded in the signals.
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Citations
10 Claims
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1. An apparatus for processing data, sent from a satellite in the form of a fixed frequency signal containing phase modulated pulse doublets or orbit definition data, to determine a position of a vehicle on the earth, comprising:
- a. receiver means for receiving the signal from the satellite, said receiver means comprising;
1. intermediate frequency means for domodulating the fixed frequency signal for processing;
2. phase detector means for determining the phase of the demodulated signal from said intermediate frequency means;
3. phase lock loop means receiving an output of said phase detector means for regulating the frequency of said intermediate frequency means;
4. doppler demodulator means responsive to an output of said phase lock loop means for determining the doppler shift in frequency of the signal sent from the satellite;
5. local oscillator means for forming a reference frequency signal;
6. synthesizer means for forming demodulating frequency signals for said intermediate frequency means, said phase detector means, and said doppler demodulator means from said reference frequency signal;
7. bit phase detector means for determining the phase of the orbit definition data phase doublets;
8. bit rate phase lock loop means for contrOlling the phase of the orbit definition data pulse doublets; and
9. data decoder means for decoding the orbit definition data from the phase modulated pulse doublets;
b. computer means for processing the doppler shift and orbit definition data to determine the location of the vehicle;
c. interface circuit means for providing the doppler shift and orbit definition data to said computer means, said interface circuit means including doppler counter means for counting the doppler shift; and
d. display means for indicating the location of the vehicle determined by said computer means.
- a. receiver means for receiving the signal from the satellite, said receiver means comprising;
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2. phase detector means for determining the phase of the demodulated signal from said intermediate frequency means;
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3. The structure of claim 1, further including:
- tape reader means for reading an operation controlling program into said computer means.
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4. doppler demodulator means responsive to an output of said phase lock loop means for determining the doppler shift in frequency of the signal sent from the satellite;
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5. The structure of claim 1, wherein said interface circuit means further includes:
- data multiplexer means for multiplexing the decoded orbit description data and the doppler count from said doppler counter means for processing by said computer means.
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6. synthesizer means for forming demodulating frequency signals for said intermediate frequency means, said phase detector means, and said doppler demodulator means from said reference frequency signal;
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7. The structure of claim 6, wherein said interface circuit means comprises:
- message reject means for suppressing output signals from said data decoder means in response to a message reject signal from said computer means.
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8. bit rate phase lock loop means for contrOlling the phase of the orbit definition data pulse doublets;
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9. The structure of claim 8, wherein said receiver means includes:
- counter means for counting a predetermined number of valid data before transmitting such data to said computer means.
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10. The structure of claim 1, further including:
- means for entry of data and requests therefor into said computer means.
Specification