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Overview of GPS

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PRN number. Sometimes referred to as Precise Positioning Service (PPS) ... Radio interference. Ionospheric disturbance. Receiver dynamics. Receiver malfunction ... – PowerPoint PPT presentation

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Title: Overview of GPS


1
Overview of GPS
2
GPS Signal Frequency
  • Fundamental Frequency 10.23MHz (f0)
  • 2 Carrier Frequencies
  • L1 (1575.42 MHz) (154 f0)
  • L2 (1227.60 MHz) (120 f0)
  • 2 Codes
  • Coarse Acquisition (C/A) 1.023 MHz
  • Precise (P) 10.23 MHz
  • Spread Spectrum
  • Harder to jam

3
Frequency and Wavelength
c vl Where c speed of light in vacuum,
2.9979246x108 m/s v frequency l
wavelength E.G. Thermal IR, l 12x10-6 m What
is frequency, v? 2.9979246x108 m/s v (12x10-6
m) v 2.49827x1013 s-1 25x1012 s-1 25
terahertz
4
Amplitude Modulation
5
Frequency Modulation
6
Phase Modulation
7
Codes
  • Stream of binary digits known as bits or chips
  • Sometimes called pseudorandom noise (PRN) codes
  • Code state 1 and 1
  • C/A code on L1
  • P code on L1 and L2
  • Phase modulated

8
C/A Code
  • 1023 binary digits
  • Repeats every millisecond
  • Each satellite assigned a unique C/A-code
  • Enables identification of satellite
  • Available to all users
  • Sometimes referred to as Standard Positioning
    Service (SPS)
  • Used to be degraded by Selective Availability (SA)

9
P Code
  • 10 times faster than C/A code
  • Split into 38 segments
  • 32 are assigned to GPS satellites
  • Satellites often identified by which part of the
    message they are broadcasting
  • PRN number
  • Sometimes referred to as Precise Positioning
    Service (PPS)
  • When encrypted, called Y code
  • Known as antispoofing (AS)

10
Future Signal
  • C/A code on L2
  • 2 additional military codes on L1 and L2
  • 3rd civil signal on L5 (1176.45 MHz)
  • Better accuracy under noisy and multipath
    conditions
  • Should improve real-time kinematic (RTK) surveys

11
Time Systems
  • Each satellite has multiple atomic clocks
  • Used for time and frequency on satellite
  • GPS uses GPS Time
  • Atomic time started 6 January 1980
  • Not adjusted for leap seconds
  • Used for time tagging GPS signals
  • Coordinated Universal Time (UTC)
  • Atomic time adjusted for leap seconds to be
    within 0.9 s of UT1 (Earth rotation time)

12
Pseudorange Measurements
  • Can use either C/A- or P-code
  • Determine time from transmission of signal to
    when the signal is received
  • Distance timespeed of light
  • Since the position of the satellite is assumed to
    be known, a new position on the ground can be
    determined from multiple measurements

13
Carrier-phase Measurements
  • The range is the sum of the number of full cycles
    (measured in wavelengths) plus a fractional cycle
  • ? N? n ?
  • The fraction of a cycle can be measured very
    accurately
  • Determining the total number of full cycles (N)
    is not trivial
  • Initial cycle ambiguity
  • Once determined, can be tracked unless

14
Cycle Slips
  • Discontinuity or jump in phase measurements
  • Changes by an integer number
  • Caused by signal loss
  • Obstructions
  • Radio interference
  • Ionospheric disturbance
  • Receiver dynamics
  • Receiver malfunction

15
How to Fix Cycle Slips?
  • Slips need to be detected and fixed
  • Triple differences can aid in cycle slips
  • Will only affect one of the series
  • Should stand out
  • Once detected, it can be fixed

16
GPS Errors and Biases
  • Satellite Errors
  • Potentially different for each satellite
  • Transmission Errors
  • Depends on path of signal
  • Receiver Errors
  • Potentially different for each receiver

17
Linear Combination
  • Errors and biases, which cannot be modeled,
    degrade the data
  • Receivers that are close enough have very
    similar errors and biases
  • Data can be combined in ways to mitigate the
    effects of errors and biases

18
Linear Combination
  • Combine data from two receivers to one satellite
  • Should have same satellite and atmospheric errors
  • Differences should cancel these effects out

19
Linear Combination
  • Combine data from one receiver to two satellites
  • Should have same receiver and atmospheric errors
  • Differences should cancel these effects out

20
Linear Combination
  • Combine data from two receivers to two satellites
  • Should have same receiver, satellite and
    atmospheric errors
  • Differences should cancel out

21
Linear Combination
  • Can also combine the L1 and L2 data to eliminate
    the effects of the ionosphere
  • Ionosphere-free combination
  • L1 and L2 phases can also be combined to form the
    wide-lane observable
  • Long wavelength
  • Useful in resolving integer ambiguity
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