Channel Modeling ETIN10. Wireless Positioning

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Channel Modeling ETIN10 Lecture no: 10 Wireless Positioning Fredrik Tufvesson Department of Electrical and Information Technology 2014-03-03 Fredrik Tufvesson - ETIN10 1

Overview Motivation: why wireless positioning? Core principles for wireless positioning Satellite positioning systems GPS Summary 2014-03-03 Fredrik Tufvesson - ETIN10 2

Why are we interested in wireless positioning? Because there are a multitude of applications: Network organization, e.g., self-organizing sensor networks Location-specific services, e.g., billing, advertisement Guiding applications, e.g., augmented reality Tracking applications, e.g., players in sports Automation and control, e.g., forklifts in industry To mention a few 2014-03-03 Fredrik Tufvesson - ETIN10 3

Core principles for wireless positioning 2014-03-03 Fredrik Tufvesson - ETIN10 4

Classical navigation 2014-03-03 Fredrik Tufvesson - ETIN10 5

Errors in angle translate to position error 2014-03-03 Fredrik Tufvesson - ETIN10 6

Self- and remote-positioning Starting point: Several units with fixed positions and a single mobile unit with unknown coordinates Self-(contained) positioning Fixed units transmit mobile unit measures Pros: Works with existing wireless networks; integrity Cons: Accuracy limited by complexity of mobile unit Remote positioning Mobile unit transmit fixed units measure Pros: Mobile device can be small and cheap Cons: Requires backbone network; integrity There are also indirect versions of both (position estimated at one side then shared with the other) 2014-03-03 Fredrik Tufvesson - ETIN10 7

Techniques for wireless positioning Three main measurement principles: Angle-of-arrival (AOA) Received signal strength (RSS) Propagation-time: Time-of-arrival (TOA) Roundtrip-time-of-flight (RTOF) Time-difference-of-arrival (TDOA) These differ both in terms of system requirements and in accuracy 2014-03-03 Fredrik Tufvesson - ETIN10 8

Angle-of-arrival (AOA) based positioning Fixed unit Fixed unit α β Based on bearing estimation followed by intersection of different direction pointers Requires antenna arrays or directive antennas at measuring side: requires complex hardware Accuracy limited by size of antenna array or directivity No requirements on synchronization Mobile unit 2014-03-03 Fredrik Tufvesson - ETIN10 9

Received signal strength (RSS) based positioning Fixed unit P(d 1 ) P(d 2 ) Fixed unit Based on propagation-loss equations Propagation-loss is often more complex than free-space (1/d^2) loss, e.g., indoors Advanced models required Mobile unit Fingerprinting (learn actual field strength from measuerements) Feasible implementation: Most radio modules already provide an RSS indicator 2014-03-03 Fredrik Tufvesson - ETIN10 10

Time-based positioning: Time-of-arrival (TOA) Fixed unit τ 1 τ 2 Fixed unit Mobile unit Based on one-way propagation time Requires precise synchronization of all involved units (time synchronization directly affects accuracy) Ex. A 1 ns clock drift implies a distance error of 0.3 m Bandwidth dependent (accuracy inversely proportional to bandwidth) Can provide higher accuracy than AOA and RSS methods 2014-03-03 Fredrik Tufvesson - ETIN10 11

Time-based positioning: Roundtrip-time-of-flight (RTOF) Fixed unit 2τ 1 2τ 2 Fixed unit Mobile unit Based on roundtrip time (RTT) Lower requirements on synchronization than TOA, but depends on delay/processing time of responder Ex. Processing time of 1 ms can lead to an error of several meters Bandwidth dependent 2014-03-03 Fredrik Tufvesson - ETIN10 12

Time-based positioning: Time-difference-of-arrival (TDOA) Fixed unit Backbone network τ 1 +δ τ 1 Fixed unit Based on the difference in time-of-arrival measured in several pairs of measuring units Only receive units needs to be synchronized Handled by backbone network for remote-positioning Bandwidth dependent Mobile unit 2014-03-03 Fredrik Tufvesson - ETIN10 13

GPS 2014-03-03 Fredrik Tufvesson - ETIN10 14

GPS Global Positioning System Started in 1978 Operational in 1993 Each satellite continually transmits messages that include the time the message was transmitted precise orbital information the general system health and rough orbits of all GPS satellites (the almanac). 2012-02-27 Fredrik Tufvesson - ETIN10 15

Satellites 24 sattelites at 20 000 km above earth Orbits with a period of 11 hours 58 minutes, in order to always follow the same track on the earth surface. 2014-03-03 Fredrik Tufvesson - ETIN10 16

Satellite track 2014-03-03 Fredrik Tufvesson - ETIN10 17

2014-03-03 Fredrik Tufvesson - ETIN10 18

Solution: We need 4 satellites to get a position in three dimensions. If we have access to more signals, we can correct for errors in the local clock. 2014-03-03 Fredrik Tufvesson - ETIN10 19

Uncertainty in position: Dilution of precision (DOP) 2014-03-03 Fredrik Tufvesson - ETIN10 20

Error PDF (Probability Density function) Probability(Error < Distance) 1.00 0.90 0.80 0.70 0.60 0.50 0.40 0.30 0.20 0.10 Measured distribution 30 days data Fix every 2 seconds MEASURED AND MODELED DISTRIBUTION OF HORIZONTAL ERRORS Garmin emap (GA-27C antenna) Modeled distribution (based on measured 4.01 m RMS error) Error Meas. Pred. 50% (CEP) 2.9 m 3.3 m Mean 3.3 m 3.6 m RMS 4.0 m (meas.) 95% 6.9 m 7.0 m 99% 10.1 m 8.6 m 0.00 0.0 5.0 10.0 15.0 Distance [meters] 2014-03-03 Fredrik Tufvesson - ETIN10 21

Indoor GPS 2014-03-03 Fredrik Tufvesson - ETIN10 22

Train station 2014-03-03 Fredrik Tufvesson - ETIN10 23

Local transmitters: 2014-03-03 Fredrik Tufvesson - ETIN10 24

L1 L2 L3 L4 L5 1575.42 MHz 1227.60 MHz 1381.05 MHz 1379.913 MHz 1176.45 MHz 2014-03-03 Fredrik Tufvesson - ETIN10 25

Link Budget example Satellite TX: 14.3 dbw ( 27 W) Satellite antenna gain: +13.4 db Polarization mismatch loss: 3.4 db Path loss: 184.4 db Atmospheric attenuation: 2.0 db Recieve antenna gain: 3.0 db Power at reciever input: -160 dbw (10-16 W) 2014-03-03 Fredrik Tufvesson - ETIN10 26

Spectral power density of recieved signal 2014-03-03 Fredrik Tufvesson - ETIN10 27

2014-03-03 Fredrik Tufvesson - ETIN10 28

Code acquisition Satellite speed: 7000 km/h Doppler shift: -6000 to +6000 Hz 2014-03-03 Fredrik Tufvesson - ETIN10 29

Spectral power density of corr. signal 2014-03-03 Fredrik Tufvesson - ETIN10 30

2014-03-03 Fredrik Tufvesson - ETIN10 31

Base station positioning 2014-03-03 Fredrik Tufvesson - ETIN10 32

WiFi positioning 2014-03-03 Fredrik Tufvesson - ETIN10 33

GPS risks 2014-03-03 Fredrik Tufvesson - ETIN10 35