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Chapter 10

Global Positioning System (GPS)

Syllabus & Marks Distribution

DetailInformation
Chapter10 — GPS (Global Positioning System)
Teaching Hours4 hours
Marks Allocation6 marks
Total Course Marks80 marks
Weight7.5% of total

Syllabus Topics

  • Basic concept of GPS
  • How GPS works
  • DGPS (Differential GPS)
  • Errors in GPS
  • Application

Importance & Frequently Asked Topics HIGH

Marks Distribution by Each Exam

Asked 17 times across past exams. Total marks: 92. Average marks per exam: ~6.

ExamMarks
2071 Bhadra6
2071 Magh9
2072 Ashwin8
2072 Magh6
2073 Bhadra6
2073 Magh6
2074 Bhadra2
2074 Magh4
2075 Bhadra6
2075 Magh9
2076 Bhadra6
2078 Chaitra7
2079 Chaitra6
2080 Chaitra3
2081 Chaitra—
2082 Shrawan8

Frequently Asked Topics

TopicTimes AskedFrequency
How GPS Works 10
Errors in GPS 7
Basic Concept of GPS 5
Application 2
DGPS 1

Topic-wise Importance & Exam Tips

TopicImportanceKey Points / Exam Tips
How GPS works (trilateration principle)HighExplain with diagram: 1 satellite = sphere, 2 = circle, 3 = two points, 4th resolves ambiguity + clock error. Three segments of GPS.
Errors in GPSHighList all error sources with magnitude. Know ionospheric delay (~5m), tropospheric (~0.5m), multipath (~1m), ephemeris (~2.5m). GDOP/PDOP concept.
DGPS (Differential GPS)HighExplain principle: base station computes corrections, transmits to rover. Real-time vs post-processing DGPS. Accuracy improvement.
Applications of GPSMediumList 6-8 applications with brief descriptions. GPS integration with GIS for field data collection.
GPS segments (Space, Control, User)MediumDescribe each segment with components. Number of satellites, orbital parameters, ground stations.
GPS vs DGPS comparisonMediumComparison table covering accuracy, cost, equipment, and applications of standalone GPS vs DGPS.

1. The Three Main Components (Segments) of GPS

PAST EXAM QUESTIONS ON THIS TOPIC:

  1. Explain the components of a GPS [4] (2071 Magh, Q5a)
  2. Explain about the components of GPS [3] (2076 Bhadra, Q4a)
  3. Explain the functions of GPS segments [3] (2075 Bhadra, Q10a)
  4. Discuss the main components of a GPS system. Explain the roles of the space segment, control segment and user segment in GPS system. (2082 Shrawan)
  5. Discuss the main components of a GPS system. Explain the roles of the space segment, control segment and user segment in GPS system. (2082 Shrawan)

The Global Positioning System consists of three interactive segments that work together to provide location, velocity, and timing information anywhere on Earth.

Space Segment 24+ NAVSTAR Satellites 6 orbital planes · ~20,200 km altitude Control Segment Ground Stations & MCS Monitor • Calculate • Upload User Segment GPS Receivers (passive) Phone • Survey rover • Navigation Signal broadcast Monitor signals ⬆ Upload corrections [X] No direct link Minimum 4 satellites visible from any point on Earth at all times
Fig 10.1 – The Three Segments of GPS: Space, Control, and User

GPS System Overview (Lectures pp.31–32)

GPS is a radio navigation system used on land, sea, and air to determine exact location, time, and velocity irrespective of weather conditions. First used by the US military in the 1960s.

Three parts:

  1. Satellites: Act like stars in constellations, constantly sending out signals from known positions.
  2. Ground stations: Use radar to verify that satellites are where they should be.
  3. Receivers: Devices (in phones, cars, survey equipment) that constantly listen for satellite signals and calculate distance from four or more satellites to determine position.

A. The Space Segment

B. The Control Segment

C. The User Segment

2. Advantages and Disadvantages of GPS (3 Marks)

PAST EXAM QUESTIONS ON THIS TOPIC:

  1. Write short notes on: Advantages and disadvantages of GPS [3] (2071 Magh, Q6d)

If asked for short notes on the pros and cons use these distinct technical and practical points.

Advantages:

  1. Global & Continuous Availability: It provides highly accurate positioning navigation and timing (PNT) data 24 hours a day 7 days a week anywhere in the world.
  2. Weather Independent: Unlike traditional optical surveying (like using a Total Station) GPS radio waves can penetrate clouds rain and snow allowing for work in any weather condition.
  3. High Precision for Engineering: Advanced techniques like DGPS or RTK (Real-Time Kinematic) can achieve sub-centimeter accuracy revolutionizing highway alignment dam monitoring and topographical surveying.
  4. Unlimited Users: Because the system is one-way (satellites broadcast users only receive) an infinite number of people can use the system simultaneously without overloading it.

Disadvantages:

  1. Requires Clear Line of Sight: GPS signals cannot easily penetrate solid objects. It fails or severely degrades indoors underground in dense forests (canopy effect) or in cities with tall buildings (the "urban canyon" effect).
  2. Susceptible to Interference: The radio signals from the satellites are very weak by the time they reach Earth. They can be easily disrupted by atmospheric interference (ionospheric delays) intentional jamming or spoofing.
  3. Battery Dependency: User receivers require continuous power to track satellites and process data which can be a limitation during remote field surveys.
  4. GPS: Advantages vs Disadvantages Advantages + 24/7 global coverage any weather + Sub-cm accuracy with DGPS/RTK + Unlimited users (passive receivers) + No intervisibility required (vs Total Station) + Works in rain snow fog clouds Radio signals penetrate atmosphere Disadvantages - Fails indoors underground dense forest - Multipath errors near tall buildings - Atmospheric delays degrade accuracy - Battery-dependent receivers - Vulnerable to jamming / spoofing Needs clear sky view to 4+ satellites
    Fig 10.2 – GPS advantages and disadvantages: strengths in coverage and weather independence vs limitations in urban canyons and indoors

10.2

Part 1: Basic Principles and How GPS Works (Trilateration)

PAST EXAM QUESTIONS ON THIS TOPIC:

  1. Explain Basic Principles of GNSS. [4] (2074 Magh, Q4b)
  2. Explain the guiding principles of GPS measurement with descriptive figures [3] (2073 Bhadra, Q4a)
  3. How does the GPS work? [4] (2078 Chaitra, Q4b)
  4. Describe briefly on how GPS works? [3] (2075 Bhadra, Q10b)
  5. Explain how GPS can find position of a point [6] (2072 Magh, Q11)
  6. Illustratively explain how position is determined using GPS [Part of 6] (2073 Magh, Q8)

1. The Basic Principle: Trilateration

GPS determines position using a mathematical principle called 3D Trilateration. Unlike triangulation (which measures angles), trilateration measures distances from known points (the satellites) to find an unknown point (the receiver).

2. How GPS Finds a Position (Step-by-Step):

  1. Signal Transmission: A GPS satellite broadcasts a radio signal containing its exact location in space and the precise time the signal left the satellite.
  2. Distance Calculation (Ranging): The GPS receiver on the ground catches this signal. It compares the time the signal was transmitted with the time it arrived. By multiplying this time delay by the speed of light (c = 3×108 m/s), the receiver calculates its exact distance from that satellite.
    Distance = Speed of Light × Time Delay
  3. The Intersection of Spheres (The Illustration):
    • 1 Satellite: Knowing the distance from one satellite places the receiver somewhere on the surface of an enormous imaginary sphere.
    • 2 Satellites: The intersection of two spheres creates a 2D circle of possible locations.
    • 3 Satellites: Adding a third sphere intersects that circle at exactly two discrete points. (One point is usually deep in space or moving impossibly fast, so the receiver easily discards it).
    • 4 Satellites: A fourth satellite is required to perfectly confirm the correct 3D point (Latitude, Longitude, Altitude) and, crucially, to correct the clock error in the user's receiver.
① One Satellite S1 = Sphere ② Two Satellites = Circle ③ Three Satellites ← discard = 2 Points ④ Four Satellites Fix [OK] 3D Position Lat, Lon, Alt = Exact Point Progressive sphere intersection narrows location to a single 3D point 4th satellite also corrects receiver clock error (Δt)
Fig 10.3 – GPS Trilateration: Progressive intersection of satellite spheres to determine position

Why 4 Satellites? (Lectures p.34)

Each satellite’s distance measurement places the receiver on a sphere centred on that satellite. With 2 satellites, the intersection is a circle. With 3 satellites, intersection narrows to 2 possible points. The 4th satellite resolves the ambiguity and gives the exact 3D position. The 4th satellite also corrects the receiver’s clock error (the “clock bias” unknown).

Part 2: The Basic Equation of GPS (The Pseudorange Equation)

PAST EXAM QUESTIONS ON THIS TOPIC:

  1. Explain basic principles and basic equation of GPS [2] (2071 Bhadra, Q8b)
  2. Explain basic principles of GNSS and basic equation of GNSS [4] (2075 Magh, Q4c)

Because the clock in your GPS receiver is not perfectly synchronized with the atomic clocks on the satellites, the distance measured is not perfectly accurate. We call this estimated distance the Pseudorange.

To get full marks, you must write the fundamental equation used to solve for the receiver's position.

The Pseudorange Equation:

The pseudorange equation relates the measured distance to the geometric distance plus clock bias and atmospheric errors.

The Mathematical Rule:

Looking at the equation, we have four unknowns: Xr, Yr, Zr, and dt. In algebra, to solve for four unknowns, you must have a system of at least four independent equations. This is the mathematical reason why you must have a minimum of 4 satellites locked to get a true GPS position.

The Pseudorange Equation (Annotated) Pi = √[(Xi−Xr)² + (Yi−Yr)² + (Zi−Zr)²] + c·dt Pⁱ = Pseudorange Measured (imperfect) distance Xⁱ, Yⁱ, Zⁱ Satellite position (known) Xᵣ, Yᵣ, Zᵣ Receiver position (UNKNOWN) c · dt = Clock Bias c = speed of light (3×10⁸) dt = receiver clock error (UNKNOWN) 4 unknowns (Xᵣ, Yᵣ, Zᵣ, dt) -> Need minimum 4 satellite equations to solve
Fig 10.4 – The Pseudorange Equation: each term annotated showing known satellite positions, unknown receiver position, and clock bias

Part 3: How Time is Maintained in GPS/GNSS

PAST EXAM QUESTIONS ON THIS TOPIC:

  1. Write short notes on: How the time is maintained in GPS [2] (2074 Bhadra, Q6ii)
  2. How time is maintained in GNSS? [2] (2075 Magh, Q4d)

Time is the absolute most critical component of GNSS. Because radio waves travel at the speed of light (300,000 km per second), a clock error of just 1/1,000,000 of a second (one microsecond) translates to a positioning error of 300 meters on the ground!

Here is how the system maintains perfect time:

  1. Atomic Clocks in Space: Every GPS satellite is equipped with highly precise, multi-million dollar atomic clocks (usually Rubidium or Cesium). These clocks are so stable they only lose or gain a fraction of a second over millions of years.
  2. Master Control Updates: Even atomic clocks experience slight drifts due to relativity (moving fast in orbit makes time pass differently than on Earth). The Master Control Station continuously monitors these clocks and uploads daily correction parameters to the satellites.
  3. Receiver Clock Synchronization: Consumer GPS receivers (like your phone or a survey rover) cannot afford atomic clocks; they use cheap, standard quartz clocks which are notoriously inaccurate.
  4. The Mathematical Fix: When the receiver locks onto the 4th satellite, it treats its own clock inaccuracy (Δt) as an algebraic unknown. The internal processor simultaneously solves the four pseudorange equations, perfectly calculating the exact time delay. In doing so, it mathematically forces the cheap quartz clock to perfectly synchronize with the satellite's atomic GPS time.
  5. How GPS Maintains Perfect Time Satellite Atomic Clock (Rubidium/Cesium) Accuracy: 1ns/day ±0.3m error/day Control Station Monitors drift Computes corrections Uploads daily updates + Relativity corrections Receiver Quartz Clock (cheap, inaccurate) Syncs via 4th satellite Solves dt algebraically Synchronized GPS Time ±10 nanoseconds Critical Fact: 1 μs clock error = 300 m position error This is why the 4th satellite is essential — it solves the receiver clock bias algebraically
    Fig 10.5 – GPS time chain: atomic clocks in satellites -> monitored by control -> receiver syncs via 4th satellite equation

Part 1: Differential GPS (DGPS)

PAST EXAM QUESTIONS ON THIS TOPIC:

  1. Explain Principal of DGPS [2] (2071 Bhadra, Q8c)

DGPS Accuracy (Lectures p.32)

Standard GPS provides accuracy of about 10 metres. DGPS improves this to approximately 1 metre, and with advanced techniques can achieve 10 cm or better. DGPS uses a fixed base station at a known position to calculate real-time corrections, which are then applied to the rover receiver’s measurements. Note: DGPS corrections improve position accuracy only and have no effect on speed-based results.

1. The Principle of DGPS (2 Marks)

Base Station Known coordinate Computes error Δ True − Observed = Correction Rover Field receiver Applies correction Radio: Correction Factor (ΔX, ΔY, ΔZ) Common-mode error cancellation: same atmosphere → same error → correction works Result: sub-meter to centimeter precision for engineering surveys
Fig 10.6 – DGPS Principle: Base Station at known point broadcasts corrections to Rover

2. Why do we need DGPS even with sophisticated GPS systems? (3 Marks)

Even the most advanced, expensive autonomous GPS receiver cannot defeat physics. Standard GPS signals must travel through 20,000 km of space and the Earth's atmosphere.

Part 2: Errors in GPS and Their Corrections

PAST EXAM QUESTIONS ON THIS TOPIC:

  1. Explain different types of errors in GPS [2] (2071 Bhadra, Q8a)
  2. Explain the possible errors that might occur while using GPS. How can accuracy of GPS be increased? [3] (2073 Bhadra, Q4b)
  3. What are the sources of error in GPS measurements? How can the accuracy be increased? [3] (2076 Bhadra, Q4b)
  4. Explain sources of errors in GPS and their corrections [8] (2072 Ashwin, Q5a)
  5. How can you use GNSS (GPS) for navigation and survey? Explain multipath error in GNSS [3+3] (2079 Chaitra, Q4a)

If an exam asks for an 8-mark breakdown of errors or how to increase accuracy, group the errors into three main categories.

1. Atmospheric Errors (The Biggest Natural Source)

Atmospheric Error Details (Lectures p.33)

Ionospheric delay: GPS signals pass through the ionosphere (outer atmosphere), where solar radiation causes particles to split and become positively charged. This introduces the largest delay — up to 16 ns, causing up to 5 m positional error. The delay varies with receiver location, satellite position, time of day, and solar flare activity.

Tropospheric delay: The “weather” layer of the atmosphere (clouds, rain, lightning) adds a smaller delay of up to 1.5 ns, causing up to 0.5 m positional error.

These delays are random and fluctuating. Each delay is satellite-specific since signals from different satellites traverse different atmospheric paths.

2. System and Satellite Errors

3. Site and Receiver Errors

GPS Error Sources & Their Corrections Error Source Magnitude Cause Correction Method Ionospheric Delay ±5m Charged particles slow signal in ionosphere Dual-frequency receivers (L1+L2) Tropospheric Delay ±0.5m Water vapor & temperature bend signal Atmospheric models + DGPS Satellite Clock Drift ±2m Atomic clock imperfections Control segment uploads corrections Ephemeris Error ±2.5m Predicted orbit ≠ actual orbit position Precise ephemeris + DGPS Multipath ±1m Signal bounces off buildings/surfaces Choke-ring antenna + site selection Receiver Noise ±0.3m Electronic noise in receiver hardware Better hardware + averaging TOTAL (Standalone) ±11m Combined without correction DGPS reduces to ±0.5–2m
Fig 10.8 – GPS Error Sources: magnitude, cause, and correction methods. DGPS eliminates common-mode errors
Dilution of Precision (DOP): Satellite Geometry Matters Good Geometry (Low DOP) S1 S2 S3 S4 Small error zone DOP = 1–2 (Excellent) Poor Geometry (High DOP) S1 S2 S3 S4 Large error zone DOP = 6+ (Poor)
Fig 10.9 – DOP: well-spread satellites give precise fixes (low DOP); clustered satellites produce large position uncertainty

Part 3: Navigation vs. Surveying (3 Marks)

PAST EXAM QUESTIONS ON THIS TOPIC:

  1. How can you use GNSS (GPS) for navigation and survey? Explain multipath error in GNSS [3+3] (2079 Chaitra, Q4a)

The 2079 exam asked how GNSS/GPS usage differs between navigation and surveying.

Navigation-Grade vs Survey-Grade GPS Navigation Grade • Accuracy: 3–10 meters • Single-frequency (L1 only) • Real-time, autonomous positioning • No post-processing needed Use Cases: Car navigation, hiking, delivery tracking, fleet management, smartphone location Cost: $100–$500 Survey Grade (DGPS/RTK) • Accuracy: 1–5 cm (RTK) • Dual-frequency (L1 + L2) • Base station + rover setup • Post-processing or RTK correction Use Cases: Cadastral surveys, road design, bridge construction, dam monitoring, earthwork Cost: $10,000–$50,000+ VS
Fig 10.10 – Navigation GPS (meters) vs Survey-grade RTK GPS (centimeters): accuracy, cost, and use case comparison

1. Applications of GNSS (Global Navigation Satellite System)

PAST EXAM QUESTIONS ON THIS TOPIC:

  1. Write down the applications of GNSS [3] (2075 Magh, Q4e)

To secure full marks, categorize the applications so the examiner sees the breadth of your knowledge. GNSS (which includes GPS, Galileo, GLONASS, etc.) is used across various sectors:

A. Surveying and Mapping

B. Civil Engineering and Construction

C. Navigation and Transportation

D. Precision Agriculture

E. Timing and Synchronization

2. Advantages and Limitations of Smartphone Apps for GNSS Field Survey (3 Marks)

PAST EXAM QUESTIONS ON THIS TOPIC:

  1. Discuss the advantages and limitations of using smartphone apps for GNSS -based field survey [3] (2080 Chaitra, Q6)

With the rise of apps like SW Maps, QField, or Avenza, smartphones are increasingly used for preliminary field surveys. However, they cannot replace professional survey rovers for engineering work.

Advantages:

  1. Cost-Effective: Eliminates the need to buy 10,000+ survey-grade equipment for simple data collection tasks. The hardware is already owned, and the apps are often free or low-cost.
  2. High Portability and Ease of Use: No need to carry heavy tripods, base stations, or external batteries. The intuitive touch interfaces make training field workers extremely fast.
  3. Instant Cloud Integration: Smartphones have built-in cellular data (4G/5G), allowing surveyors to instantly upload collected points, photos, and attribute data directly to a central GIS server in real-time.

Limitations:

  1. Poor Accuracy: Standard smartphone GNSS chips generally provide 3 to 10 meters of accuracy. This is strictly unacceptable for civil engineering design, cadastral mapping, or earthwork calculations, which require centimeter-level precision.
  2. Weak Antennas (Multipath Susceptibility): Smartphones lack the advanced "choke-ring" antennas found on professional gear. They suffer massively from multipath errors in "urban canyons" (tall buildings) or under dense forest canopies.
  3. Battery Drain: Running the screen at full brightness while continuously tracking GNSS satellites drains a smartphone battery in just a few hours, limiting full-day field operability.
Smartphone GNSS vs Professional Survey Rover Feature Smartphone (SW Maps, QField) Survey Rover (RTK/DGPS) Accuracy 3 – 10 meters 1 – 5 centimeters Cost Free – $50 (app) $10,000 – $50,000+ Antenna Built-in patch (multipath prone) Choke-ring / geodetic grade Frequency Single-freq (L1 only) Dual-freq (L1 + L2) Battery 2–4 hours (screen + GPS) 8–12 hours (dedicated) Best For Reconnaissance, POI collection Engineering design, cadastral survey Smartphone GNSS is suitable for preliminary surveys only; engineering work requires RTK/DGPS precision
Fig 10.12 – Smartphone vs survey rover comparison: accuracy, cost, antenna quality, and appropriate use cases

Smartphone Apps for GNSS-Based Field Survey

Modern smartphones contain built-in GNSS receivers that can be used for basic field surveys using apps like SW Maps, Locus GIS, QField, and ArcGIS Field Maps.

AdvantagesLimitations
Low cost — no need for expensive survey-grade receiversLow accuracy (3–10m) — not suitable for precision surveys
Widely available — almost everyone has a smartphoneSingle-frequency receiver — cannot correct ionospheric errors
Easy to use — minimal training requiredShort battery life during continuous GNSS logging
Built-in camera for geotagged photosNo external antenna — poor signal under canopy or in urban canyons
Real-time data upload via mobile internetLimited data storage compared to dedicated survey equipment
Integration with GIS apps (QField, ArcGIS Field Maps)No post-processing capability for differential correction
Good for reconnaissance surveys and community mappingNot accepted for legal/cadastral surveys requiring cm-level accuracy

Chapter Summary

This chapter covers the Global Positioning System (GPS), a satellite-based navigation system providing precise location and time information anywhere on Earth. The basic concept involves a constellation of satellites (minimum 24, currently 31+) orbiting at ~20,200 km altitude in 6 orbital planes. How GPS works: a receiver measures the time delay of signals from at least 4 satellites and uses trilateration to compute 3D position (latitude, longitude, altitude). The three GPS segments are: Space (satellites), Control (ground monitoring stations), and User (receivers). DGPS (Differential GPS) uses a base station at a known location to compute correction signals, improving accuracy from ~5-10m to sub-meter or even centimeter level. Errors in GPS include satellite clock errors, ephemeris errors, ionospheric and tropospheric delays, multipath errors, receiver noise, and geometric dilution of precision (GDOP/PDOP). Applications span surveying, navigation, GIS data collection, precision agriculture, fleet management, disaster response, and geodetic control networks.