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Chapter 9 of 9

Total station, GPS & remote sensing techniques

In the TNPSC AE Civil syllabus under Engineering Survey · 3 parts

📑 Contents (20 sections)

Part 1 of 3

EDM & Total Station

Last reviewed 16 Sept 2026 · 8 min read

Electronic distance measurement (EDM)

EDM measures distances by electromagnetic waves instead of tapes. It gives high accuracy over long distances quickly, across rough terrain, rivers and traffic.

Principle — phase comparison

A carrier wave (microwave, infrared or light) is modulated with a measuring wave of known wavelength . The wave travels from the instrument to a reflector and back (double path). The instrument measures the phase difference between transmitted and received waves, which gives the fractional part of a wavelength (); the integer number of wavelengths () is resolved by transmitting several frequencies.

FormulaEDM distance (phase comparison)

Velocity of electromagnetic waves in air: ( = speed of light in vacuum, = refractive index of air), and .

Pulse (time-of-flight) method — the time taken by a short laser pulse to travel to the target and back gives — used in reflectorless EDM and laser scanners.

Types of EDM

Type Carrier Range and features Examples (historical)
Microwave instruments Microwaves (cm wavelengths) Long range (tens of km); work in fog/haze; need instruments at both ends (master and remote); affected by humidity Tellurometer
Visible light instruments Modulated visible light Medium to long range; affected by daylight Geodimeter
Infrared instruments Infrared (near-IR) with prism reflectors Short to medium range (a few km); compact; widely used in total stations Distomat series
Laser (reflectorless) instruments Visible or IR laser Measure to natural surfaces without a prism over limited ranges; pulse or phase methods Modern total stations, laser distance meters

Reflectors

  • Corner cube prisms (retro-reflectors) return the beam parallel to its incoming direction — single or multiple prisms for longer ranges; mounted on poles or tribrachs.
  • Reflective sheets (targets) for short ranges; reflectorless measurement to walls, rock faces and inaccessible points.
  • Each prism has a prism constant (offset) that must be set in the instrument.

Errors and corrections

Error Description / correction
Zero (additive) error / instrument constant Offset of the electrical centre from the mechanical centre of the instrument and reflector — determined by calibration on a baseline and applied as a constant
Prism constant Offset due to prism geometry — entered into the instrument
Scale error Due to frequency drift of the oscillator — proportional to distance (ppm); checked by calibration
Cyclic error Periodic error within a wavelength due to electronic interference — calibrated
Atmospheric error Refractive index of air depends on temperature, pressure (and humidity for microwaves) — correction in ppm computed from measured temperature and pressure and entered in the instrument
Centring and pointing errors At instrument and reflector — careful setup, optical/laser plummets
Multipath Reflections from nearby surfaces (especially microwaves)

Accuracy specification: stated as — a constant part plus a part proportional to distance (e.g. ±(2 mm + 2 ppm)).

Reductions

EDM measures slope distance . With the zenith angle (or vertical angle ):

Further reductions: to mean sea level (or ellipsoid) and to the map projection grid (scale factor) for control surveys.

Total station

A total station is an integrated electronic surveying instrument combining:

  1. An electronic (digital) theodolite — measures horizontal and vertical angles electronically.
  2. An EDM — measures slope distances.
  3. A microprocessor — computes horizontal distances, height differences, coordinates, etc.
  4. Data storage — internal memory, cards or data collectors, with USB/Bluetooth transfer.
  5. Display and keyboard (often both faces) with onboard software programs.
  6. Laser plummet, electronic level (dual-axis tilt compensator), guide lights.

Functions and onboard programs

Function Use
Angle and distance measurement Horizontal angle, vertical/zenith angle, slope, horizontal and vertical distances
Coordinate measurement Direct computation of E, N and Z of observed points
Stake-out (setting out) Guides placement of points of known coordinates on the ground — construction layout
Resection (free station) Determining instrument position by observing known points
Remote elevation measurement (REM) Heights of inaccessible points (e.g. power lines, bridge soffits)
Missing line measurement (MLM) Distance and height difference between two observed points
Area and volume computation From observed boundary points
Offset measurements, tie distance, traverse, road design programs Various field tasks

Setting up and orientation

  1. Set up the tripod over the station; centre with the laser/optical plummet.
  2. Level using the circular bubble and electronic level (tilt compensator corrects residual tilt).
  3. Enter station data — station coordinates, instrument height, prism height, prism constant, atmospheric correction (temperature and pressure).
  4. Orientation (backsight) — sight a known backsight point (or enter a known azimuth) to set the horizontal circle to the correct bearing.
  5. Measure detail/control points or stake out.
FormulaCoordinates from total station observations

With horizontal distance , azimuth (whole circle bearing) , vertical difference , instrument height and target (prism) height :

  • Robotic (motorised) total stations — automatic target recognition and tracking; one-person operation, machine control.
  • Reflectorless total stations — measure to surfaces without prisms.
  • Imaging total stations — integrated cameras for documentation and photogrammetric measurement.
  • Terrestrial laser scanners — capture dense point clouds (millions of points) for 3D modelling, as-built surveys, heritage documentation.
  • Integration with GNSS ("smart stations") and CAD/GIS/BIM software.

Advantages and limitations

Advantages Limitations
High accuracy and speed High cost; requires trained personnel
Automatic recording — eliminates booking errors Dependent on batteries and electronics
Computations in the field (coordinates, areas, stake-out) Line of sight required between instrument and target
Easy data transfer to computers, CAD and GIS Atmospheric and prism settings must be correct; errors can be hidden in automated outputs
Works on difficult terrain and long distances Instrument calibration needed periodically

Applications

Topographic and detail surveys; control traverses; construction layout (buildings, bridges, highways, tunnels); cadastral boundary surveys; deformation monitoring of dams, bridges, slopes and buildings; as-built surveys; volume computations of stockpiles and excavations; mining; accident reconstruction.

Part 2 of 3

Global Positioning System (GPS/GNSS)

Last reviewed 16 Sept 2026 · Facts as of 16 Sept 2026 · 8 min read

Global navigation satellite systems (GNSS)

GNSS is the general term for satellite systems that provide positioning, navigation and timing worldwide.

System Operator Key features
GPS (NAVSTAR) United States Satellites in 6 orbital planes inclined at about 55°, altitude about 20 200 km, orbital period about 12 hours (11 h 58 min); a minimum of 24 satellites (more are operational)
GLONASS Russia 3 orbital planes inclined at about 64.8°, altitude about 19 100 km
Galileo European Union 3 orbital planes inclined at about 56°, altitude about 23 200 km; civilian-controlled
BeiDou (BDS) China Mixed constellation of medium Earth orbit, geosynchronous and geostationary satellites
NavIC (IRNSS) India (ISRO) Regional system with satellites in geostationary and geosynchronous orbits, covering India and a region of about 1500 km around it
QZSS Japan Regional augmentation/complementary system

Satellite-based augmentation systems (SBAS) improve accuracy and integrity using geostationary satellites and ground reference stations — e.g. GAGAN (GPS Aided GEO Augmented Navigation, developed by ISRO and AAI for India), WAAS (USA), EGNOS (Europe).

Segments of GPS

  1. Space segment — the constellation of satellites broadcasting signals, with precise atomic clocks.
  2. Control segment — a master control station (in Colorado, USA), monitor stations and ground antennas that track satellites, compute orbits (ephemerides) and clock corrections, and upload navigation messages.
  3. User segment — receivers (navigation, mapping and geodetic/survey-grade) and antennas that compute position, velocity and time.

Signals

  • Carrier frequencies (GPS): L1 = 1575.42 MHz, L2 = 1227.60 MHz, L5 = 1176.45 MHz.
  • Codes: C/A (coarse/acquisition) code — civilian code on L1; P(Y) code — precise (encrypted military) code on L1 and L2; modernised civil codes L2C and L5.
  • Navigation message — satellite ephemeris (precise orbit), almanac (approximate orbits of all satellites), clock corrections, ionospheric model parameters, health status.

Principle of positioning

Pseudorange (code) positioning

The receiver measures the travel time of the signal from satellite to receiver:

( ≈ 299 792 458 m/s.) This measured range is called a pseudorange because the receiver clock is not synchronised with satellite clocks.

  • Each pseudorange defines a sphere centred on the satellite; the position lies at the intersection (trilateration).
  • Four unknowns — X, Y, Z coordinates and receiver clock bias — so at least four satellites must be observed simultaneously.
  • A receiver clock error of just 1 microsecond corresponds to a range error of about 300 m — hence the clock bias must be solved.

Carrier-phase positioning

The receiver measures the phase of the carrier wave (wavelength about 19 cm for L1). The integer number of cycles between satellite and receiver (integer ambiguity) is unknown and must be resolved; once fixed, carrier phase gives millimetre to centimetre relative accuracy — the basis of survey-grade GNSS. Cycle slips (loss of lock) must be detected and repaired.

Sources of error

Error Description / mitigation
Satellite clock error Corrected by broadcast clock parameters; eliminated in differential methods
Orbit (ephemeris) error Differences between predicted and actual orbits; precise ephemerides for post-processing
Ionospheric delay Signal delay by free electrons in the ionosphere — largest error source for single-frequency receivers; dual-frequency observations largely eliminate it
Tropospheric delay Delay in the lower atmosphere (dry and wet components) — modelled; larger at low elevation angles
Multipath Signals reflected from buildings, water, vehicles reach the antenna — choose open sites, choke-ring antennas, elevation mask
Receiver noise Instrumental noise
Antenna phase centre variation Calibrated antennas; consistent antenna orientation
Selective availability Deliberate degradation of civilian accuracy by the US — discontinued in May 2000
Satellite geometry Expressed by dilution of precision (DOP)

Dilution of precision

DOP measures how satellite geometry amplifies measurement errors:

  • GDOP (geometric), PDOP (3D position), HDOP (horizontal), VDOP (vertical), TDOP (time).
  • Low DOP = good geometry (satellites well spread across the sky); high DOP (satellites clustered) = poor accuracy.
  • Position error ≈ DOP × range measurement error.
  • Vertical accuracy is usually poorer than horizontal accuracy because satellites are above the horizon only.

Positioning methods

Method Description Typical accuracy
Absolute (single point) positioning One receiver, code pseudoranges Several metres
Differential GPS (DGPS) A base station at a known point computes pseudorange corrections and transmits them to rovers Sub-metre to a few metres
Static relative positioning Two or more receivers observe simultaneously for long sessions (e.g. an hour or more); carrier phase post-processed Millimetres to a centimetre — control networks, deformation monitoring
Rapid (fast) static Shorter sessions with good geometry and dual frequency Centimetre level over short baselines
Kinematic (stop-and-go) Rover moves after initialisation; carrier phase maintained Centimetre level
Real-time kinematic (RTK) Base station transmits carrier-phase corrections by radio or internet (NTRIP) to the rover; ambiguities fixed in real time About 1–2 cm horizontal (short baselines) — stake-out, detail surveys, machine control
Network RTK / CORS A network of continuously operating reference stations generates corrections over a region — no own base needed Centimetre level
Precise point positioning (PPP) Single receiver with precise orbit and clock products, dual frequency Decimetre to centimetre after convergence

The Survey of India operates a CORS network providing real-time corrections for high-accuracy positioning across the country.

Part 3 of 3

Remote Sensing & GIS

Last reviewed 16 Sept 2026 · Facts as of 16 Sept 2026 · 9 min read

Remote sensing

Remote sensing is the science of obtaining information about objects or areas on the earth's surface without physical contact, by detecting and analysing electromagnetic radiation reflected or emitted by them — usually from aircraft or satellites.

The remote sensing process

  1. Energy source (sun or the sensor itself).
  2. Radiation and the atmosphere — scattering and absorption on the way down and up.
  3. Interaction with the target — absorption, transmission, reflection, emission.
  4. Recording by the sensor.
  5. Transmission, reception and processing at ground stations.
  6. Interpretation and analysis.
  7. Application — maps, decisions.

Electromagnetic spectrum

Region Wavelength (approx.) Use
Ultraviolet < 0.4 µm Limited (atmospheric scattering)
Visible — blue, green, red 0.4–0.7 µm Natural colour images, water, vegetation, urban features
Near infrared (NIR) 0.7–1.3 µm Vegetation vigour (high reflectance), water boundaries
Short-wave infrared (SWIR) 1.3–3 µm Soil and vegetation moisture, minerals
Thermal infrared (TIR) about 3–14 µm (8–14 µm window common) Surface temperature, heat islands, fires
Microwave about 1 mm – 1 m RADAR — all-weather, day–night imaging

Atmospheric windows — wavelength ranges where the atmosphere is relatively transparent (visible, parts of IR, thermal window, microwaves); sensors operate in these windows.

Spectral signatures

Different materials reflect differently across wavelengths:

  • Healthy vegetation — low reflectance in blue and red (absorbed by chlorophyll), a peak in green, and very high reflectance in NIR (leaf structure).
  • Water — low reflectance, especially absorbs NIR strongly (appears dark in NIR images); turbid water reflects more in visible.
  • Soil — reflectance generally increases with wavelength; decreases with moisture and organic matter.
FormulaNormalised Difference Vegetation Index

Ranges from −1 to +1: dense healthy vegetation gives high positive values; bare soil near zero; water negative.

False colour composite (FCC) — standard FCC displays NIR as red, red as green and green as blue, so vegetation appears red.

Passive and active sensors

  • Passive sensors — record natural energy (reflected sunlight or emitted thermal radiation): multispectral scanners, cameras, thermal sensors. Depend on sunlight (for reflected bands) and clear skies.
  • Active sensors — emit their own energy and record the return:
    • RADAR / SAR (synthetic aperture radar) — microwave; penetrates clouds; works day and night; used for flood mapping, soil moisture, deformation (InSAR).
    • LiDAR (light detection and ranging) — laser pulses; very accurate elevation data, vegetation structure, DTMs.

Platforms and orbits

  • Ground-based, airborne (aircraft, drones) and spaceborne (satellites) platforms.
  • Geostationary orbit — about 35 786 km above the equator; satellite appears fixed relative to earth; continuous coverage of a large area — weather and communication satellites.
  • Sun-synchronous polar orbit — low altitude (typically about 600–900 km), near-polar; passes over a place at the same local solar time — earth resources satellites.

Resolutions

Resolution Meaning
Spatial Smallest object size distinguishable — pixel size on the ground (e.g. sub-metre to hundreds of metres)
Spectral Number and width of spectral bands — panchromatic (one broad band), multispectral (few bands), hyperspectral (hundreds of narrow bands)
Radiometric Sensitivity to differences in energy — number of brightness levels, for an -bit sensor (8-bit = 256 levels)
Temporal Revisit time — frequency of imaging the same area

Indian remote sensing programme

  • IRS-1A (1988) was India's first operational remote sensing satellite; the Indian Remote Sensing (IRS) series has grown into one of the largest civilian constellations.
  • Missions include Resourcesat (natural resources), Cartosat series (high-resolution stereo imagery for cartography), Oceansat (ocean studies), RISAT (radar imaging), and others.
  • The National Remote Sensing Centre (NRSC), Hyderabad, acquires, processes and distributes data; the Bhuvan geoportal provides Indian satellite imagery and thematic maps.

Image interpretation and processing

Elements of visual interpretation

Tone/colour, size, shape, texture, pattern, shadow, and site/association (location relative to other features).

Digital image processing

  1. Pre-processing:
    • Radiometric correction — sensor errors, atmospheric effects, illumination.
    • Geometric correction (georeferencing) — removing distortions and registering to map coordinates using ground control points; resampling (nearest neighbour, bilinear, cubic convolution).
  2. Image enhancement — contrast stretching, filtering (smoothing, edge enhancement), band ratios, principal components, colour composites.
  3. Image classification:
    • Supervised — analyst defines training sites; algorithms such as maximum likelihood, minimum distance, parallelepiped, and machine-learning classifiers.
    • Unsupervised — computer groups pixels into clusters (e.g. ISODATA, k-means), which the analyst labels.
    • Object-based classification — segments images into objects.
  4. Accuracy assessment — error (confusion) matrix, overall accuracy, producer's and user's accuracy, kappa coefficient.
  5. Change detection — comparing images of different dates.

Geographic Information System (GIS)

A GIS is a computer-based system to capture, store, query, analyse and display geographically referenced (spatial) data together with their attributes.

Components

Hardware, software, data (spatial and attribute), people and methods/procedures.

Data models

Vector data model Raster data model
Features represented by points, lines and polygons with coordinates Space divided into a grid of cells (pixels), each with a value
Precise boundaries; good for discrete features (roads, parcels, pipes) Good for continuous data (elevation, rainfall, imagery)
Compact storage; topology (connectivity, adjacency, containment) supports network analysis Simple structure; easy overlay and map algebra
Complex overlay operations Large storage; resolution-dependent accuracy
  • Attribute data — stored in tables linked to features (database management systems); queried with SQL-like commands.
  • TIN (triangulated irregular network) — vector representation of surfaces.

Data input

Digitising paper maps, scanning and vectorisation, GNSS/total station field data, remote sensing imagery, existing digital data (CAD, census tables), LiDAR point clouds. Metadata describes source, accuracy, projection and date.

Coordinate systems and projections

All data must share a coordinate reference system: geographic (latitude/longitude on a datum such as WGS 84) or projected (e.g. UTM zones — eastings and northings in metres). Georeferencing registers scanned maps and images to real-world coordinates.

Spatial analysis

Operation Example
Query (attribute and spatial) Find all parcels larger than 1 ha within a ward
Buffer Zone within 100 m of a river or highway
Overlay (union, intersect, clip, erase) Combine soil, slope and land use layers for site suitability
Network analysis Shortest path, service areas, facility location (ambulance, schools)
Interpolation Surfaces from point data — inverse distance weighting (IDW), kriging, spline
Terrain analysis Slope, aspect, hillshade, viewshed, watershed and drainage delineation from DEMs
Map algebra / raster calculation Weighted overlay, cost-distance, suitability indices
Proximity and density analysis Nearest facility, hot spots

Digital elevation models

DEM (bare-earth elevations, also DTM) and DSM (surface including buildings and trees). Sources: contours, stereo photogrammetry, LiDAR, radar interferometry — e.g. SRTM (about 30 m global), CartoDEM (from Cartosat stereo data).

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