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The purpose of this section is to provide an overview of GPS receiver operation The objective is to provide a su cient understanding to enable the discussion in the subsequent sections Modern receivers have several channels each capable of tracking a single CDMA signal The receiver schedules measurements from all the tracking channels to occur simultaneously according to the receivers indicated time r (t) Throughout this chapter the symbols r (t) and s (t) will be used to represent the receiver and satellite indicated times at GPS time t When multiple satellites or receivers are being discussed, s and r can be considered as counters over the set of satellites or receivers The signal broadcast by GPS satellite s has the form y( s ) = C s ( s )Ds ( s ) sin(2 fc s ) where C s is the PRN code assigned to the satellite, Ds is the bit sequence containing the 50 Hz data, and sin(2 fc s ) is the carrier signal All of these signals are generated according to the satellite time s (t) which is distinct for each satellite due to clock drift as discussed in Section 842 When the PRN for an available satellite is assigned to a GPS receiver channel, the receiver channel performs the following functions: generates a replica of the PRN code sequence; searches for the code phase and Doppler frequency to align the replica PRN code with the PRN code of the incoming signal; and, then adjusts channel variables to maintain the alignment of the incoming and generated PRN codes Typically, during tracking, the PRN code alignment can be maintained to less than 1% of one PRN code chip (< 3m) The receiver channel will also manipulate channel variables to acquire and track either the frequency or phase of the sinusoidal carrier of the signal at the channel input See Section 849 At the receiver indicated time r (t), for each channel, the basic channel measurements are: s (t ts ) the time of transmission of the signal by the satellite, as r marked on the signal (eg, tow, z-count) and tracked by the phase of the code generator (ie, integer and fractional chip count); r (t) the receiver indicated time; ca ( r (t)) the fractional portion of the phase carrier accumulator; and Nca ( r (t)) the whole cycle count of the phase carrier accumulator In the above expressions, t is the GPS system time and ts is the signal r transit time from the satellite to the receiver.

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From these basic measurements, various other measurements can be computed All measurements computed from the basic channel measurements will be referred to as observables The transit (pseudo) time, code pseudorange and phase observables are constructed as r ts r (t) s r s r r (t) r (t) = = = r (t) s (t ts ), seconds r s r (t) , meters c tr Nca r (t) + ca r (t) , cycles (822) (823) (824)

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where c is the speed of light in a vacuum Note that the transit time ts r is not directly measured, but is computed from the basic measurements For a two frequency GPS receiver each of the above observables can be computed for each of the carrier frequencies Each carrier frequency for each satellite requires its own tracking channel (ie, 12 channels to track both L1 and L2 signals for six SV s) The pseudorange observable has been discussed extensively in Section 82 Its error model is presented in eqn (86) and the use of the pseudorange observable to determine position is discussed in Section 822 Subsection 831 presents the error model for the carrier phase observable Subsection 832 discusses another receiver output often called the Doppler or deltapseudorange

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