Method and apparatus for deriving pseudo range from earth-orbiting satellites
AssigneeIstac, Incorporated
InventorsPeter F. MacDoran, Donovan J. Spitzmesser
Life of this patent
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AssigneeIstac, Incorporated
InventorsPeter F. MacDoran, Donovan J. Spitzmesser
Estimating the term…
The invention permits a user to derive his pseudo range from earth-orbiting, signal-transmitting satellites without knowledge of the code sequence of modulation carried by the signal, if any. A modulated radio frequency signal having a component at a given frequency, which is transmitted from a satellite is intercepted at a user position. The component is recovered from the intercepted signal. The phase and frequency of the component are measured. From these measurements and similar measurements from other such satellites, the pseudo range of the satellite can be derived. Specifically, a fractional phase is derived from the measured phase and frequency of the intercepted signal. A Doppler range value is also derived from the measured frequencies of the satellites. The Doppler range value is divided by the wavelength of the given frequency to produce an integer and a remainder. The integer is added to the fractional phase to produce a value proportional to the pseudo range.
A method for deriving pseudo range from a user to earth-orbiting, signal-transmitting satellites that transmit a radio frequency signal having a component at a given frequency, the method comprising the steps of:
A method for deriving pseudo range from a user to a signal transmitting satellite that transmits a radio frequency signal having a first component at a given frequency and a second component at a frequency higher than the given frequency, the method comprising the steps of:
A method of deriving pseudo range from a user to a plurality of signal transmitting satellites that transmit radio frequency signals having a component at a given frequency, the method comprising the steps of:
Dependencies are inferred from the claim text.