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newSchoolWorks.com › VoTechWorks › Technology & Design › GIS / Surveying / Drone Operations › GNSS Field Operations and Data Processing › Lesson 1
TEC-GIS45-03 · Lesson 1 · 10 clock hours · theory

GNSS Fundamentals and Satellite Constellation Overview

Objective. Students will correctly describe how GPS, GLONASS, Galileo, and BeiDou constellations provide positioning and explain the role of satellite geometry (DOP values) in accuracy.

⚠ Pending professional review

This lesson, its worked examples and its practice questions has not yet been verified by an industry-certified professional or by a certification or approval body. It is a study draft and may contain errors. Do not use it as instructions for work on a job site or on live equipment. Always follow your instructor, your supervising professional, and current official references and regulations.

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What Is GNSS?

Global Navigation Satellite System (GNSS) is the umbrella term for any satellite-based positioning system. The United States GPS (Global Positioning System) is the oldest and most widely used, but three other fully operational constellations now serve the industry: Russia's GLONASS, the European Union's Galileo, and China's BeiDou (also called BDS). Modern survey-grade and drone-grade receivers track signals from multiple constellations simultaneously, which increases the number of visible satellites at any moment and improves both accuracy and reliability.

The Four Major Constellations

GPS is operated by the U.S. Department of Defense. The constellation is designed to maintain at least 24 operational satellites in medium Earth orbit (MEO) at roughly 20,200 km altitude, arranged in six orbital planes. GPS broadcasts on the L1 (1575.42 MHz), L2 (1227.60 MHz), and L5 (1176.45 MHz) frequency bands.

GLONASS is operated by the Russian Aerospace Defence Forces. It also uses MEO satellites at approximately 19,100 km altitude across three orbital planes. GLONASS uses a frequency-division multiple access (FDMA) scheme, meaning each satellite transmits on a slightly different frequency, unlike GPS which uses code-division multiple access (CDMA). GLONASS signals occupy bands near L1 and L2 frequencies.

Galileo is operated by the European Union Agency for the Space Programme (EUSPA). Designed from the start as a civilian system, Galileo broadcasts on E1, E5a, E5b, and E6 bands. The E5a band overlaps with GPS L5 (1176.45 MHz), allowing receivers to combine signals for improved ionospheric correction.

BeiDou (BDS) is operated by China and uses a mixed constellation of MEO, geostationary (GEO), and inclined geosynchronous (IGSO) satellites, giving it particularly strong coverage over the Asia-Pacific region. BeiDou signals are broadcast on B1, B2, and B3 frequency bands.

Why Multiple Constellations Matter

A receiver needs signals from at least four satellites to solve for three-dimensional position (latitude, longitude, and ellipsoidal height) plus receiver clock error. Tracking more constellations means more satellites in view at all times, which is critical in urban canyons, dense forest, or when working near tall structures where some sky is blocked. More visible satellites also improve satellite geometry.

Frequency Bands and Why They Matter

GNSS receivers that track only one frequency (single-frequency, L1-only) cannot separate ionospheric delay from position error. Dual-frequency receivers (L1/L2 or L1/L5) can mathematically model and remove most of the ionospheric delay by comparing how the two signals travel differently through the ionosphere. Triple-frequency receivers add a third measurement, further improving ambiguity resolution speed and accuracy. For survey-grade work and precision drone mapping, dual- or multi-frequency receivers are the professional standard.

Error Sources in GNSS

Four main error sources affect every GNSS measurement:

1. Ionospheric delay — The ionosphere (roughly 60–1,000 km altitude) slows the signal. The effect varies with solar activity and time of day. Dual-frequency receivers correct for most of this error.

2. Tropospheric delay — The lower atmosphere (below about 50 km) also slows signals. Models and pressure/temperature sensors help reduce this error.

3. Multipath — Signals reflecting off buildings, vehicles, water, or terrain arrive at the receiver via indirect paths, corrupting the measurement. Antenna placement and choke-ring antennas reduce multipath.

4. Satellite clock and ephemeris errors — Broadcast corrections and augmentation systems (WAAS, CORS networks, RTK) reduce these to centimeter or sub-centimeter levels.

Safety note: When setting up GNSS equipment in the field, assess the site for traffic hazards, unstable terrain, and overhead power lines before placing tripods or range poles. Never set up a tall tripod or range pole near overhead power lines. If lightning threatens, cease operations, lower all poles and antennas, and move to shelter immediately — metal tripods and poles are conductive. Follow your program's PPE requirements for outdoor fieldwork including high-visibility vests near roadways.

Satellite Geometry and DOP Values

Having many satellites visible is not enough on its own — their positions in the sky matter too. Dilution of Precision (DOP) is a dimensionless number that describes how satellite geometry amplifies or reduces ranging errors. A lower DOP means better geometry and smaller position errors; a higher DOP means poor geometry and larger errors.

Common DOP components:

As a practical rule of thumb widely cited in manufacturer documentation and NGS guidance, a PDOP of 4 or less is generally acceptable for survey work; PDOP above 6 is considered poor and observations should be delayed if possible. The relationship between DOP and position error is:

Position Error ≈ DOP × User Equivalent Range Error (UERE)

If your receiver's ranging error (UERE) is 1 m and PDOP = 2, your expected position error is roughly 2 m. If PDOP rises to 6, the expected error rises to roughly 6 m — using the same equipment under the same sky.

Planning GNSS Observations

Before collecting data, especially for static control surveys, professionals use GNSS planning software to predict satellite availability and DOP values for a specific location, date, and time window. You input the site's approximate coordinates and an elevation mask angle (the minimum sky angle above which satellites are tracked — commonly 10° to 15° in open terrain to exclude low-quality, high-delay signals). The software outputs a graph of PDOP over time and a sky plot showing satellite positions. You then select the observation window when PDOP is lowest and the most satellites are visible across all constellations. This planning step directly affects data quality and is a standard professional practice.

Key terms8

GNSSGlobal Navigation Satellite System; the umbrella term for all satellite-based positioning systems including GPS, GLONASS, Galileo, and BeiDou.
L1 / L2 / L5GPS signal frequency bands broadcast at 1575.42 MHz, 1227.60 MHz, and 1176.45 MHz respectively; dual- and multi-frequency receivers use these bands together to correct ionospheric delay.
Ionospheric delayThe slowing of GNSS signals as they pass through the ionosphere; the primary ranging error source for single-frequency receivers, largely removed by dual-frequency processing.
MultipathSignal error caused by GNSS signals reflecting off surfaces and arriving at the receiver via indirect paths, distorting the measured range.
Dilution of Precision (DOP)A dimensionless multiplier that describes how satellite geometry magnifies ranging errors; lower values indicate better geometry and smaller position uncertainty.
PDOPPosition Dilution of Precision; the DOP component describing three-dimensional position quality; values of 4 or less are generally acceptable for survey work.
Elevation mask angleThe minimum sky angle above the horizon at which a receiver will track satellites; set typically between 10° and 15° to exclude low-elevation signals subject to greater atmospheric delay and multipath.
FDMA vs. CDMAFrequency-Division Multiple Access (used by GLONASS) assigns each satellite a unique frequency; Code-Division Multiple Access (used by GPS, Galileo, BeiDou) lets satellites share frequencies but uses unique codes to distinguish signals.

Worked examples3

1. A GNSS receiver has a User Equivalent Range Error (UERE) of 0.5 m. The current PDOP is 3. Estimate the expected three-dimensional position error.
  1. Recall the relationship: Position Error ≈ DOP × UERE.
  2. Substitute the known values: Position Error ≈ 3 × 0.5 m.
  3. Multiply: 3 × 0.5 = 1.5 m.
Answer: The expected 3D position error is approximately 1.5 m.
2. During the same session, a satellite configuration change causes PDOP to rise to 6. Using the same UERE of 0.5 m, what is the new expected position error, and how much larger is it than the original?
  1. Apply the formula: Position Error ≈ PDOP × UERE = 6 × 0.5 m = 3.0 m.
  2. Calculate the increase: 3.0 m − 1.5 m = 1.5 m larger.
  3. Express as a ratio: 3.0 ÷ 1.5 = 2, so the error doubled.
Answer: The new expected position error is 3.0 m, which is 1.5 m (or twice) larger than the original 1.5 m error.
3. A GNSS planning application shows two possible observation windows at a site: Window A has 9 satellites visible with a PDOP of 1.8; Window B has 5 satellites visible with a PDOP of 5.2. The project specification requires PDOP ≤ 4. Which window meets the specification, and if UERE = 0.8 m, what is the expected position error for that window?
  1. Check the specification: PDOP must be ≤ 4. Window A PDOP = 1.8 (passes); Window B PDOP = 5.2 (fails).
  2. Select Window A as the compliant window.
  3. Calculate position error for Window A: Position Error ≈ 1.8 × 0.8 m = 1.44 m.
Answer: Window A meets the specification. The expected position error during Window A is approximately 1.44 m.

The math in this lesson1

Learners estimate position error as PDOP x UERE, e.g., 3 x 0.5 m = 1.5 m.
A-SSE.1
Brush up in the math halls at newSchoolWorks.com:
In class: Guided reading and annotation of manufacturer and NGS reference materials on GNSS signal structure, frequency bands (L1, L2, L5), and constellation status; students summarize key differences between constellations in a comparison table. · Instructor-led whiteboard session tracing a GNSS signal from satellite to receiver; students draw and label the signal path, identifying ionosphere, troposphere, and multipath interference points. · Small-group exercise using a free GNSS planning application (e.g., Trimble GNSS Planning or equivalent) to evaluate DOP values and satellite availability for a given location and time window; groups present findings and justify an optimal observation window.
Materials: Projector, whiteboard, NGS 'Introduction to GNSS' publication, manufacturer receiver manual, GNSS planning software (lab computers), student notebooks
Check: Students complete a 20-question multiple-choice quiz on constellation names, frequency bands, DOP definitions, and error sources; passing score 70%.

Practice check8

Answer each question, then check it. Nothing is recorded; this is your own practice.

GNSS fundamentals / NSPS CST technical knowledge
1. Which of the following GNSS constellations is operated by the European Union?
GNSS signal processing / NSPS CST technical knowledge
2. A dual-frequency GNSS receiver is preferred over a single-frequency receiver for survey-grade work primarily because dual-frequency receivers can:
Satellite geometry and DOP / NSPS CST technical knowledge
3. What does a PDOP value of 2 indicate compared to a PDOP value of 6?
GNSS error sources / NSPS CST technical knowledge
4. Which error source is best described as signals arriving at the receiver via indirect reflections off nearby buildings or vehicles?
GNSS signal structure / FAA Part 107 airspace/technology knowledge
5. GPS broadcasts on three carrier frequency bands. Which set correctly identifies all three?
GNSS field operations / NSPS CST practical knowledge
6. An elevation mask angle of 15° means a GNSS receiver will:
GNSS constellation characteristics / NSPS CST technical knowledge
7. Which GNSS constellation uses frequency-division multiple access (FDMA), assigning each satellite its own slightly different carrier frequency?
DOP calculation and observation planning / NSPS CST practical knowledge
8. A project specification states PDOP must not exceed 4. Your GNSS planning software shows two windows: Window 1 has PDOP = 3.5 and Window 2 has PDOP = 4.8. If your UERE is 1.0 m, what is the expected position error during the compliant window?
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