GELE Geodesy — Satellite Geodesy and GNSSCheat Sheet
A printable cheat sheet for Satellite Geodesy and GNSS, built for GELE reviewers who want one go-to reference in the final stretch. Covers formulas, key definitions, common question types, and the Professional Regulation Commission (PRC) — Board of Geodetic Engineering-specific twists you will see on GELE day.
Exam context
The Geodetic Engineer Licensure Examination is conducted by Professional Regulation Commission (PRC) — Board of Geodetic Engineering and is scheduled for September 2026. The Geodesy subtest is marked as "Core" in the official pattern, and Satellite Geodesy and GNSS appears in position 6th of 6 in the GELE Geodesy review rotation. Passing mark: 70% weighted average, no sub-test below 50%. Recent GELE 2026 papers have drawn roughly a meaningful share of questions from this subject.
Satellite Geodesy and GNSS - Cheat Sheet
Your last-minute revision companion for Satellite Geodesy and GNSS. Covers positioning principles, observables, error sources, DOP, differential methods, RTK, reference frames, and all exam-critical formulas. Master this in 30 minutes before your exam.
Sections
Formulas
Formula
ρ = c × Δt
Meaning
ρ = pseudorange (m); c = speed of light (299,792,458 m/s); Δt = signal travel time (s)
Watch Out
Δt is in SECONDS, not milliseconds. Common error: forgetting c is ~3×10⁸ m/s exactly (use 299,792,458 m/s for precision)
When To Use
Calculate pseudorange from satellite signal travel time; fundamental to all GNSS positioning
Formula
X = X_sat + c × (Δt_sat - Δt_receiver)
Meaning
Solve receiver position (X, Y, Z) and clock bias using satellite ephemeris and pseudorange measurements
Watch Out
Four unknowns (X, Y, Z, Δt_receiver) require MINIMUM 4 satellites; three satellites cannot solve a 3-D fix
When To Use
Conceptual formulation of trilateration with clock bias correction
Formula
n_min = 4
Meaning
Minimum number of satellites for 3-D positioning with clock bias correction
Watch Out
Three satellites give only 2-D fix (height constrained). The fourth unknown is RECEIVER CLOCK BIAS, not a satellite
When To Use
Any exam question asking 'how many satellites do you need for a 3-D fix?'
Common Values
Value
299,792,458 m/s (≈ 3×10⁸ m/s)
Symbol
c
Quantity
Speed of light
Value
~20,200 km (semi-major axis a ≈ 26,560 km)
Symbol
h_GPS
Quantity
GPS orbital altitude
Value
~0.067 s (to ground from geosynchronous altitude)
Symbol
Δt_GPS
Quantity
Signal travel time (GPS)
Value
4
Symbol
n_min
Quantity
Minimum satellites for 3-D fix
Section Title
GNSS Positioning Principle & Fundamentals
Important Facts
- GNSS is based on TRILATERATION: measure ranges to satellites of KNOWN POSITION to solve receiver position
- Speed of light c = 299,792,458 m/s (exact, by definition)
- A 3-D fix requires MINIMUM 4 satellites (3 for position, 1 for clock bias)
- Pseudorange accuracy is typically METRES (coarse); achieved in seconds to minutes
- GPS satellites orbit at ~20,200 km altitude; signal travel time ~0.067 s
- GNSS equations are NONLINEAR; usually solved by least-squares adjustment when using >4 satellites
- Dilution of Precision (DOP) is a dimensionless geometry-only factor; accuracy = DOP × measurement error
Key Definitions
Term
Pseudorange
Example
If signal takes 0.067 s, pseudorange ≈ 20,086 km (consistent with GPS orbital altitude ~20,200 km)
Definition
Range measured by multiplying receiver clock time difference by the speed of light; called 'pseudo' because receiver clock is not synchronized with satellite atomic clock.
Term
Trilateration
Example
In 2-D: three circles intersect at a point; in 3-D with clock bias: four spheres intersect at a unique point
Definition
Geometric method of determining position by measuring distances from three or more known reference points (satellites).
Term
Receiver Clock Bias (Δt_receiver)
Example
Even with inexpensive quartz clocks, this bias (typically microseconds) translates to hundreds of metres of range error without correction
Definition
The systematic error in the receiver's internal clock relative to satellite atomic time; solved as a fourth unknown in GNSS positioning.
Term
Ephemeris
Example
GPS satellites broadcast their own ephemeris data every 2 hours; used to compute X_sat, Y_sat, Z_sat
Definition
Precise 3-D position and velocity of each satellite at a given time; broadcast by the satellite and must be known for positioning calculations.
Diagrams To Know
- Receiver and four satellites in 3-D space showing sphere intersection
- Pseudorange vs travel time relationship (ρ vs Δt graph)
- Receiver clock bias effect on position solution
Formulas
Formula
ρ_pseudorange = c × Δt
Meaning
Pseudorange (m); speed of light c; signal travel time Δt (s)
Watch Out
Pseudorange is COARSE (~1 m noise) because it depends on receiver clock accuracy; not suitable for precise work alone
When To Use
Single-frequency pseudorange positioning; DGPS and standard GPS receivers
Formula
Φ_carrier = (f/c) × ρ + N × λ + errors
Meaning
Φ = carrier phase (cycles); f = frequency; ρ = true range; N = integer ambiguity (cycles); λ = wavelength (m)
Watch Out
Ambiguity N is UNKNOWN integer; must be resolved (fixed) to use carrier phase. This is the bottleneck of precise GNSS
When To Use
Precise GNSS positioning (geodetic surveys, RTK); carrier-phase observables
Formula
λ = c / f
Meaning
Wavelength (m); c = speed of light; f = frequency (Hz)
Watch Out
GPS L1 = 1575.42 MHz → λ_L1 ≈ 0.19 m; L2 = 1227.60 MHz → λ_L2 ≈ 0.24 m
When To Use
Relate frequency to wavelength for L-band GNSS frequencies
Formula
Precision = λ / N_observable
Meaning
Carrier phase precision (m); wavelength λ; cycling ambiguity N
Watch Out
Carrier phase is PRECISE but AMBIGUOUS; pseudorange is COARSE but UNAMBIGUOUS
When To Use
Compare pseudorange (~1 m) vs carrier phase (~mm) accuracy
Common Values
Value
1575.42 MHz
Symbol
f_L1
Quantity
GPS L1 frequency
Value
0.1905 m ≈ 19.05 cm
Symbol
λ_L1
Quantity
GPS L1 wavelength
Value
1227.60 MHz
Symbol
f_L2
Quantity
GPS L2 frequency
Value
0.2442 m ≈ 24.42 cm
Symbol
λ_L2
Quantity
GPS L2 wavelength
Value
1–5 m (1-σ)
Symbol
σ_pseudorange
Quantity
Pseudorange noise (typical)
Value
2–5 mm (1-σ)
Symbol
σ_phase
Quantity
Carrier phase noise (typical)
Section Title
GNSS Observables: Pseudorange & Carrier Phase
Important Facts
- PSEUDORANGE: coarse observable (~1 m precision), unambiguous, from travel time measurement
- CARRIER PHASE: precise observable (~mm precision), ambiguous (integer ambiguity must be resolved)
- GPS L1 frequency = 1575.42 MHz (wavelength ≈ 0.19 m)
- GPS L2 frequency = 1227.60 MHz (wavelength ≈ 0.24 m)
- Dual-frequency receivers can form ionosphere-free combinations to remove first-order iono delay
- Ambiguity resolution is the key to cm-level positioning; without it, carrier phase is useless
- Cycle slips (loss of lock) cause ambiguity jumps; must be detected and repaired
Key Definitions
Term
Carrier Phase Observable
Example
GPS L1 carrier phase at 1575.42 MHz (λ ≈ 0.19 m); one cycle = 0.19 m of range
Definition
Count of whole wavelengths plus fractional phase from satellite to receiver; precision ~mm but requires integer ambiguity resolution.
Term
Integer Ambiguity (N)
Example
With 4 satellites × 2 frequencies, solve 8 ambiguities; fixing these reduces error from metres to centimetres
Definition
Unknown number of complete wavelengths between satellite and receiver at the start of tracking; resolved in post-processing or real-time via RTK.
Term
Dual-Frequency GNSS
Example
Single-frequency: ambiguity fixing takes minutes; dual-frequency: seconds to minutes
Definition
Receiver tracking two frequencies (e.g., GPS L1 and L2) to remove ionospheric delay and resolve ambiguities faster.
Diagrams To Know
- Pseudorange vs Carrier Phase observable accuracy vs time
- Integer ambiguity effect on solution convergence
- L1 and L2 frequency spectrum diagram
Formulas
Formula
Total Error = Clock Error + Orbit Error + Iono Delay + Tropo Delay + Multipath + Receiver Noise
Meaning
All systematic and random errors contribute to pseudorange/phase bias
Watch Out
Errors are NOT always additive; correlations (especially between iono and tropo) exist
When To Use
Understand error budget and why differential GNSS removes common errors
Formula
Iono Delay = 40.3 × (TEC / f²)
Meaning
TEC = Total Electron Content (electrons/m²); f = frequency (Hz); delay in metres
Watch Out
Single-frequency receivers see ~5–50 m error on L1 alone; dual-frequency reduces this to ~0.1 m
When To Use
Explain why dual-frequency receivers form ionosphere-free combinations
Formula
Tropo Delay ≈ 2.5 m at zenith (dry component)
Meaning
Depends on temperature, pressure, humidity; increases with lower elevation angle
Watch Out
Tropo is FREQUENCY-INDEPENDENT (same for L1 and L2); cannot remove by dual-frequency like iono
When To Use
Estimate systematic delay for low-elevation satellites; corrected using models (Hopfield, Saastamoinen)
Common Values
Value
~1 m
Symbol
δt_sat
Quantity
Satellite clock error (uncorrected)
Value
2–5 m
Symbol
δr_orbit
Quantity
Orbit error (broadcast ephemeris)
Value
5–50 m (varies by time of day, solar activity)
Symbol
δ_iono
Quantity
Ionospheric delay (L1, zenith)
Value
2.5 m (dry) + 0.1–0.5 m (wet)
Symbol
δ_tropo
Quantity
Tropospheric delay (zenith)
Value
1–3 m
Symbol
δ_MP_code
Quantity
Multipath (pseudorange)
Value
5–50 mm
Symbol
δ_MP_phase
Quantity
Multipath (carrier phase)
Section Title
Error Sources in GNSS
Important Facts
- SATELLITE CLOCK ERROR: ~1 m (corrected by broadcast ephemeris); residual ~0.1 m after correction
- ORBIT ERROR: ~2–5 m; reduced by precise ephemeris (IGS products ~0.05 m)
- IONOSPHERIC DELAY: 5–50 m single-frequency; removed by dual-frequency (~0.1 m residual)
- TROPOSPHERIC DELAY: 2–20 m depending on elevation; modelled, ~0.1 m residual after correction
- MULTIPATH: 1–3 m for pseudorange; 5–50 mm for carrier phase; mitigated by antenna design and environment
- RECEIVER NOISE: 1–5 m pseudorange; 2–5 mm carrier phase
- DOP multiplies measurement error: accuracy ≈ DOP × σ_measurement
- Typical DOP values: PDOP = 2–10 (PDOP < 4 is excellent; > 10 is poor)
Key Definitions
Term
Ionospheric Delay
Example
L1 (1575 MHz) sees more delay than L2 (1227 MHz); difference used to estimate and remove iono effects
Definition
Propagation delay caused by free electrons in the ionosphere; frequency-dependent, causing code/phase distortion on different frequencies.
Term
Tropospheric Delay
Example
~2.5 m at zenith; increases to ~20 m for 5° elevation angle
Definition
Propagation delay in the neutral atmosphere (troposphere); frequency-independent, caused by dry gases and water vapor.
Term
Multipath
Example
GPS receiver near building or water surface sees multipath; solution: use choke-ring antenna or move away from reflectors
Definition
Signal reflected off nearby objects before reaching antenna; creates phase distortion and range bias.
Term
Cycle Slip
Example
Typical during low elevation, obstructed sky, or receiver motion; must be detected and repaired
Definition
Loss of phase lock on satellite signal, causing discontinuity in carrier-phase count (integer ambiguity jumps by N cycles).
Term
Satellite Geometry (DOP)
Example
Satellites spread across sky → low DOP → high accuracy; satellites clustered overhead → high DOP → poor accuracy
Definition
Quality of spatial distribution of satellites; quantified by Dilution of Precision (DOP); lower DOP = better geometry.
Diagrams To Know
- Error budget pie chart (relative contributions of each error source)
- Satellite elevation vs tropospheric delay curve
- Ionospheric delay vs frequency relationship
- Multipath geometry (direct + reflected signals)
Formulas
Formula
Accuracy ≈ DOP × σ_measurement
Meaning
Accuracy (m); DOP = dimensionless geometry factor; σ = user-equivalent range error (UERE) or noise (m)
Watch Out
DOP is GEOMETRIC ONLY; does not include systematic errors (iono, tropo, orbit); this formula gives PRECISION, not ACCURACY
When To Use
Estimate positioning uncertainty from satellite geometry and receiver noise
Formula
PDOP = √(σ_X² + σ_Y² + σ_Z²)
Meaning
Position DOP; combines 3-D position uncertainty
Watch Out
PDOP includes clock uncertainty; cannot isolate horizontal/vertical separately
When To Use
Overall accuracy estimate including all coordinates
Formula
HDOP = √(σ_X² + σ_Y²)
Meaning
Horizontal DOP; includes only X and Y (horizontal plane)
Watch Out
HDOP alone does NOT tell you Z error; use VDOP for vertical or PDOP for total
When To Use
Estimate horizontal accuracy (useful for navigation, surveying horizontal control)
Formula
VDOP = σ_Z
Meaning
Vertical DOP; includes only Z (height)
Watch Out
VDOP is typically 1.5–3 times larger than HDOP due to poor vertical satellite geometry
When To Use
Estimate vertical (height) accuracy
Formula
UERE ≈ 5 m (typical single-frequency GPS, standard code)
Meaning
User Equivalent Range Error; combined pseudorange noise including all unmodelled errors
Watch Out
Can increase to 10+ m in poor conditions (low elevation, high humidity, solar activity)
When To Use
Default estimate if no other information given; scales with elevation mask and atmospheric conditions
Common Values
Value
< 4
Symbol
PDOP_excellent
Quantity
Excellent PDOP
Value
4–8
Symbol
PDOP_good
Quantity
Good PDOP
Value
8–16
Symbol
PDOP_moderate
Quantity
Moderate PDOP
Value
> 16
Symbol
PDOP_poor
Quantity
Poor PDOP
Value
1–2
Symbol
HDOP_typical
Quantity
Typical HDOP (open sky)
Value
2–4
Symbol
VDOP_typical
Quantity
Typical VDOP (open sky)
Value
5 m (1-σ)
Symbol
UERE
Quantity
Standard UERE (GPS code)
Section Title
Dilution of Precision (DOP) & Positioning Accuracy
Important Facts
- DOP is a PURE GEOMETRY FACTOR; does not include atmospheric errors, multipath, or clock bias
- Lower DOP = better (multiplies measurement error); higher DOP = worse (amplifies error)
- PDOP < 4 is EXCELLENT; PDOP 4–8 is GOOD; PDOP > 16 is POOR and should be avoided for surveys
- VDOP is always LARGER than HDOP (satellites rarely come from horizon in one direction like elevation)
- Satellites at LOW ELEVATION angles have HIGHER DOP contribution (weight less in solution)
- Elevation mask (e.g., 10°) removes low-elevation satellites but improves PDOP by excluding poor-geometry solutions
- Real-time DOP prediction via almanac allows pre-mission planning (choose time/location with good DOP)
- DOP calculations available in all survey-grade GNSS receivers; monitor during field work
Key Definitions
Term
Dilution of Precision (DOP)
Example
PDOP = 2.5 with σ = 3 m gives ~7.5 m accuracy; same σ with PDOP = 5 gives ~15 m accuracy
Definition
Dimensionless factor describing how satellite geometry affects positioning accuracy; lower DOP = better accuracy for same measurement precision.
Term
PDOP (Position DOP)
Example
Excellent: PDOP < 4; Good: PDOP 4–8; Moderate: PDOP 8–16; Poor: PDOP > 16
Definition
3-D position dilution of precision; affects accuracy of X, Y, Z, and clock bias simultaneously.
Term
HDOP (Horizontal DOP)
Example
Typically 0.8–2.5 for open sky; HDOP < 2 is considered good for surveying
Definition
Horizontal dilution of precision; affects accuracy of X and Y only (latitude and longitude).
Term
VDOP (Vertical DOP)
Example
Typically 1.5–3× larger than HDOP due to poor satellite elevation distribution (satellites overhead, not at horizon)
Definition
Vertical dilution of precision; affects accuracy of Z (height/ellipsoid height) only.
Term
UERE (User Equivalent Range Error)
Example
UERE = 5 m typical; UERE = 3 m with dual-frequency and correction models
Definition
Pseudo-range noise equivalent, combining all unmodelled systematic and random errors; typical 3–10 m for standard GPS.
Diagrams To Know
- DOP vs satellite count curve
- DOP vs elevation angle for a single satellite
- PDOP contour map over time of day
- Satellite skyplot showing good vs poor geometry
Formulas
Formula
Correction = ρ_true_reference - ρ_observed_reference
Meaning
ρ_true = known pseudorange to reference station; ρ_observed = measured pseudorange at reference; difference = error to broadcast
Watch Out
Assumes errors are CORRELATED between base and rover (true for iono/tropo/orbit within ~20–30 km); multipath is NOT correlated
When To Use
Compute correction at a base station on known point; apply to rover to remove common errors
Formula
Accuracy_rover ≈ 0.5–1 m (DGPS, static differential)
Meaning
Horizontal accuracy after differential correction; depends on baseline length and correction model
Watch Out
Accuracy DEGRADES with longer baselines (>50 km); iono/tropo decorrelation; use precise ephemeris for longer lines
When To Use
Planning survey accuracy with DGPS (Code-based differential)
Common Values
Value
5–10 m
Symbol
σ_standalone
Quantity
Standalone GPS accuracy
Value
0.5–1 m
Symbol
σ_DGPS_5km
Quantity
DGPS accuracy (5 km baseline)
Value
1–2 m
Symbol
σ_DGPS_50km
Quantity
DGPS accuracy (50 km baseline)
Value
~100 km (accuracy degrades beyond)
Symbol
L_DGPS_max
Quantity
Max practical DGPS baseline
Value
1–10 Hz
Symbol
f_corr
Quantity
Correction update rate (typical)
Section Title
Differential GNSS (DGPS) & Static Differential
Important Facts
- DGPS requires REAL-TIME or POST-PROCESSED corrections from a base station on a known point
- Error sources removed by differential: satellite clock, orbit, ionosphere, troposphere (partial)
- Error sources NOT removed: multipath (site-specific), receiver noise, baseline-dependent decorrelation
- Accuracy typically 0.5–1 m horizontal (compared to 5–10 m for standalone GPS)
- Accuracy degrades with baseline length (~5 cm/km for baseline > 50 km)
- Communication link needed for real-time DGPS (radio, cellular, internet); post-processing doesn't need real-time link
- Static differential: base and rover both stationary; corrections computed and applied in post-processing
- Kinematic differential: rover moving; corrections applied in real-time (less common than RTK now)
Key Definitions
Term
Differential GNSS (DGPS)
Example
Reference on monument broadcasts corrections; rover 20 km away applies them → accuracy improves from ~5 m to ~0.5–1 m
Definition
Technique where corrections computed at a known-position reference station are transmitted to rover receiver to remove common systematic errors.
Term
Base Station (Reference Station)
Example
Coast Guard DGPS network uses fixed reference stations to broadcast 50 Hz corrections over radio
Definition
Receiver on a point of known coordinates (from prior survey or high-order control); computes and broadcasts corrections to rovers.
Term
Rover
Example
Survey crew with rover receiver receives DGPS corrections from base on monument; position improves in real-time
Definition
Mobile receiver that applies corrections from base station to improve its own position estimate.
Term
Baseline
Example
5 km baseline: 90% error correlation; 50 km: ~70%; 100 km: ~50%
Definition
Vector distance between base and rover; errors decorrelate at longer baselines (typically >50 km for DGPS)
Diagrams To Know
- Base–rover geometry with error correlation decay vs distance
- DGPS workflow: base computes corrections → rover applies corrections → improved position
- Correction broadcast architecture (radio/cellular/internet link)
Formulas
Formula
RTK Accuracy ≈ 2–5 cm horizontal + 3–10 cm vertical (fixed integers)
Meaning
Centimetre-level accuracy for real-time positioning with carrier-phase differential and resolved ambiguities
Watch Out
Accuracy valid ONLY after ambiguity fixing (status = FIXED); before fix (FLOAT), accuracy is similar to DGPS (0.5–1 m)
When To Use
Machine guidance, stake-out, rapid control densification; only when fix status is FIXED
Formula
Ambiguity Search Space = N_sat × N_freq × (2 × max_cycle_slip + 1)
Meaning
Total integer combinations to test; N_sat = satellites, N_freq = frequencies; cycle slip ≈ 1–3 cycles typical
Watch Out
Fixing is PROBABILISTIC; low PDOP, weak signals, or multipath cause false fix (wrong integer); always validate before use
When To Use
Understand why RTK initialization takes seconds (with dual-frequency) vs minutes (single-frequency)
Formula
Time-to-Fix (s) ≈ N_ambiguities / (f_update × SNR)
Meaning
Rough estimate of convergence time; depends on receiver update rate, signal strength, and geometry
Watch Out
Poor geometry (high PDOP) or obstructed sky significantly increases time-to-fix; can exceed 5 minutes in bad conditions
When To Use
Field planning: how long to wait after initializing RTK?
Common Values
Value
2–5 cm
Symbol
σ_RTK_H
Quantity
RTK horizontal accuracy (FIXED)
Value
3–10 cm
Symbol
σ_RTK_V
Quantity
RTK vertical accuracy (FIXED)
Value
0.5–1 m
Symbol
σ_RTK_float
Quantity
RTK accuracy (FLOAT, before fix)
Value
10–30 s
Symbol
t_fix_dual
Quantity
Typical time-to-fix (dual-freq)
Value
1–5 minutes
Symbol
t_fix_single
Quantity
Typical time-to-fix (single-freq)
Value
20–50 km (standard); ~100 km with network
Symbol
L_RTK
Quantity
RTK baseline limit
Value
1–2 s
Symbol
Δt_link
Quantity
Correction link latency (max)
Section Title
Real-Time Kinematic (RTK) & Precise GNSS Methods
Important Facts
- RTK achieves 2–5 cm accuracy through CARRIER-PHASE DIFFERENTIAL + INTEGER AMBIGUITY RESOLUTION (not pseudorange alone)
- Time-to-fix varies: dual-frequency 10–30 s; single-frequency 1–5+ minutes; depends on baseline, geometry, and code/phase noise
- RTK baseline typically limited to 20–50 km (network RTK extends this via regional base stations)
- Ambiguity fixing is PROBABILISTIC; false fixes possible if PDOP poor or multipath severe; validate with redundant observations
- Loss of lock (cycle slip) reverts status to FLOAT; automatic re-initialization usually 5–30 s; must monitor skyplot during dynamic survey
- Dual-frequency receivers fix ambiguities ~10× faster than single-frequency (iono elimination reduces noise)
- Real-time requirement: correction link latency must be < 1–2 s; satellite geometry must remain stable during fix hold
- RTK is now dominant method for control densification and stake-out in Philippines; replaces classical surveying
Key Definitions
Term
Real-Time Kinematic (RTK)
Example
Construction equipment or survey drone uses RTK for autonomous stake-out; position updates 1–20 Hz at cm accuracy
Definition
Real-time carrier-phase differential GNSS with integer ambiguity resolution, providing cm-level positioning without post-processing.
Term
Fixed Solution (Fix)
Example
After initialization, receiver enters FIXED mode; accuracy typically 2–5 cm if geometry and signal strength remain good
Definition
Integer ambiguities are resolved to integers with high confidence; solution has cm-level accuracy.
Term
Float Solution (Float)
Example
During RTK initialization, receiver shows FLOAT status with ~0.5 m accuracy; once fixed, jumps to 2–5 cm
Definition
Ambiguities solved as real numbers (not integers) via least-squares; accuracy similar to DGPS (0.5–1 m); lower than FIXED.
Term
Ambiguity Initialization / Time-to-Fix
Example
Dual-frequency: 10–30 s typical; single-frequency: 1–5 minutes or longer
Definition
Time required to resolve integer ambiguities from FLOAT to FIXED status; depends on geometry, satellite count, and baseline.
Term
RTK Network (RTN)
Example
Philippines: PRISM (PRS-based RTN) provides coverage; single rover connects to nearest base instead of owning base station
Definition
Regional network of fixed base stations (e.g., CORS) that compute and transmit real-time corrections via wireless link.
Term
NTRIP (Network Transport of RTCM via Internet Protocol)
Example
Receiver connects via cellular/WiFi to NTRIP server; receives RTK corrections and achieves cm accuracy
Definition
Standard protocol for distributing GNSS correction data (RTCM) over internet to mobile receivers; enables internet-based RTK.
Diagrams To Know
- RTK workflow: base tracks satellites → computes ambiguities and corrections → rover initializes and fixes → cm-level positioning
- Fix/Float transition during RTK survey
- Time-to-fix vs baseline length curve
- NTRIP architecture and mobile RTK network diagram
Formulas
Formula
Accuracy ≈ 5 mm + 1 ppm × baseline
Meaning
Typical accuracy after post-processing static survey with dual-frequency carrier phase; 5 mm fixed error + 1 ppm of baseline length
Watch Out
Assumes good geometry, minimal multipath, and convergence; poor conditions can degrade to 1–2 cm
When To Use
Estimate precision of baseline after post-processing (e.g., survey network, control densification)
Formula
Session Duration ≥ (10 + baseline_km) minutes
Meaning
Rough rule-of-thumb for static observation duration to achieve ambiguity resolution and stable solution
Watch Out
Modern dual-freq receivers with good sky view can fix faster (5–10 min for 20 km); poor geometry requires longer
When To Use
Plan field sessions: 5 km line needs ~15 min; 50 km needs ~60 min
Common Values
Value
5 mm + 1 ppm baseline
Symbol
σ_static
Quantity
Static survey accuracy (dual-freq)
Value
1–2 cm + 1 ppm
Symbol
σ_rapidstatic
Quantity
Rapid-static accuracy
Value
30 min (10 km baseline); 2–4 h (100 km)
Symbol
t_session
Quantity
Typical static session duration
Value
5–10 min (dual-freq, good sky)
Symbol
t_min_fix
Quantity
Minimum session for ambiguity fix
Section Title
Post-Processing & Static Surveys
Important Facts
- Post-processing can achieve 5 mm + 1 ppm accuracy (much better than real-time RTK) due to precise ephemeris use
- Static survey minimum 30 minutes typical; longer sessions (2–4 hours) improve reliability and reduce systematic errors
- Rapid-static (5–10 min) with dual-frequency sufficient for many surveys; single-frequency may need 30+ min for reliable fix
- Kinematic processing requires good initialization (5 min + static at start, or fixed ambiguities from prior baseline)
- Cycle slips in kinematic must be detected and repaired; modern software handles this automatically
- Multi-system (GPS + GLONASS + Galileo + BeiDou) significantly improves convergence speed and reliability
- Processing software (Leica Infinity, Trimble Business Centre, RTKLIB, Bernese) all use least-squares adjustment
- Control network adjustment ties multiple baselines together; distributes errors; improves closure
Key Definitions
Term
Static Survey
Example
Survey crew occupies point A for 30 minutes (carrier phase), then point B for 30 minutes; baseline A–B computed with 5–10 mm accuracy
Definition
Both receiver and surveyor remain stationary during session; processed in post-processing mode; highest accuracy (~5 mm + 1 ppm).
Term
Rapid-Static
Example
Quick control densification: occupy each point 10 min with modern receiver → 1–2 cm accuracy, much faster than traditional static
Definition
Shortened static session (5–10 min) with dual-frequency receiver and resolved ambiguities; accuracy ~1–2 cm.
Term
Kinematic Survey
Example
Drone surveys: fly trajectory while tracking; post-process to get cm-level orthophoto/DTM
Definition
Rover moves along trajectory while tracking satellites; processed in post-processing; intermediate accuracy (few cm) if well-initialized.
Term
Post-Processing
Example
Collect 2-hour static session on 100 km baseline; download precise ephemeris; post-process offline; achieve 5–10 mm accuracy
Definition
GNSS data processing done after field session complete; uses stored raw observations and precise ephemeris; no real-time correction link needed.
Diagrams To Know
- Static survey session plan (two points, observation times)
- Baseline processing workflow: raw data → ambiguity fixing → least-squares → coordinates
- Convergence curve: RMS error vs observation duration
- Network adjustment diagram (multiple baselines, control points)
Formulas
Formula
WGS84 (World Geodetic System 1984)
Meaning
Geocentric reference frame fixed to Earth's center of mass; origin at Earth's centre; Z-axis toward North Pole; X-axis toward 0° meridian/equator
Watch Out
WGS84 ≠ PRS92; difference up to ~1 m in Philippines; must apply transformation to comply with RA 8560
When To Use
All GPS/GNSS measurements are computed in WGS84; must transform to local datum (PRS92) for Philippine surveys
Formula
PRS92 (Philippine Reference System 1992) based on Clarke 1866 ellipsoid
Meaning
Local datum for Philippines; uses Clarke 1866 ellipsoid (a = 6378206.4 m, e² ≈ 0.00674); fixed to monument constellation
Watch Out
Never use WGS84 directly for Philippine property or engineering surveys; VIOLATION of RA 8560 and RA 4374
When To Use
All Philippine land surveys, property deeds, engineering projects must use PRS92 coordinates and monuments
Formula
WGS84 to PRS92 transformation: Δ E ≈ −127.5 m, Δ N ≈ −116 m (rough, Luzon region)
Meaning
Approximate shift between WGS84 and PRS92 in Philippines; varies by region (Visayas, Mindanao differ)
Watch Out
Official PRS92–WGS84 transformation uses 7-parameter Helmert or region-specific grids (BX files); do NOT use simple shift
When To Use
Quick sanity check: if WGS84 and PRS92 differ by >2 m, check transformation parameters
Common Values
Value
6378137 m
Symbol
a_WGS84
Quantity
WGS84 semi-major axis
Value
1/298.257
Symbol
f_WGS84
Quantity
WGS84 flattening
Value
6378206.4 m
Symbol
a_Clarke
Quantity
Clarke 1866 (PRS92) semi-major axis
Value
ΔE ≈ −127.5 m, ΔN ≈ −116 m
Symbol
δ_LuzonShift
Quantity
WGS84–PRS92 shift (Luzon, approx)
Value
1992 (frozen; no plate motion updates)
Symbol
t_PRS92
Quantity
PRS92 epoch
Value
5–10 cm/year
Symbol
v_plate
Quantity
Typical plate motion (Philippines)
Section Title
Reference Frames: WGS84, PRS92, ITRF
Important Facts
- All GNSS results are computed in WGS84 or ITRF (geocentric frame); LOCAL DATUM (PRS92) required for Philippine land surveys by law
- WGS84 ≠ PRS92: difference typically 1–2 m in Philippines; use PROPER TRANSFORMATION, not informal shift
- RA 8560 and RA 4374 mandate PRS92 for all surveys, cadastral records, property transactions in Philippines
- PRS92 monuments (NAMRIA benchmarks) define the local datum; all surveys tied to these monuments
- ITRF is more accurate than WGS84 but also constantly updates (ITRF2000 → 2005 → 2008 → 2014 → 2020); modern use ITRF2014/2020
- Transformation methods: 7-parameter Helmert (precise, rigorous); 3-parameter (faster, less precise); grid shift files (NAMRIA BX files)
- PPCS (Philippine Plane Coordinate System) uses PRS92 and UTM projection; coordinates in metres on local plane
- DO NOT mix frames: WGS84 + PRS92 data in same project invalidates results; always transform to common frame
Key Definitions
Term
WGS84 (World Geodetic System 1984)
Example
GPS satellite ephemeris in WGS84; raw receiver coordinates in WGS84; must transform to PRS92 for Philippine use
Definition
Geocentric reference frame (origin at Earth's centre); global standard for GNSS. Uses WGS84 ellipsoid (a = 6378137 m; f = 1/298.257).
Term
PRS92 (Philippine Reference System 1992)
Example
Property deed coordinates in PRS92; survey monuments in PRS92; engineering design in PRS92
Definition
Local datum for Philippines; fixed to monuments (NAMRIA control points); uses Clarke 1866 ellipsoid; required by law (RA 8560, RA 4374).
Term
ITRF (International Terrestrial Reference Frame)
Example
IGS precise ephemeris and station coordinates in ITRF; permanent monitoring stations track plate tectonics
Definition
Global, high-precision geocentric frame; multiple realizations (ITRF2000, 2005, 2008, 2014, 2020); supercedes WGS84 for geodetic work.
Term
Datum Transformation / Shift
Example
WGS84 → PRS92: apply 7-param transform or NAMRIA grid; PRS92 → WGS84: inverse transform
Definition
Mathematical conversion between two reference frames; 7-parameter (Helmert) transform or region-specific grid shift (BX file).
Term
Plate Tectonics & Frame Realization
Example
PRS92 coordinates valid for 1992 epoch; Philippine monument at 0° has drifted ~1 m by 2024; modern surveys use dynamic WGS84 or PRS92/2015 variant
Definition
Earth's crust moves ~5–10 cm/year; ITRF realizations updated every ~3–5 years; PRS92 fixed to historical epoch (1992) → accumulates ~1 m drift.
Diagrams To Know
- WGS84 vs PRS92 vs ITRF sphere/ellipsoid visual comparison
- 3-D transformation flow: WGS84 (raw GNSS) → ITRF → PRS92 → PPCS (plane coordinates)
- Map showing WGS84–PRS92 shift vectors across Philippines regions (Luzon, Visayas, Mindanao)
- PRS92 monument network distribution across Philippines
Common Values
Value
24–30 (typically 31–33 active)
Symbol
n_GPS
Quantity
GPS satellites
Value
24 (3 orbital planes × 8 satellites)
Symbol
n_GLONASS
Quantity
GLONASS satellites
Value
30 (24 active + 6 backup)
Symbol
n_Galileo
Quantity
Galileo satellites
Value
30+ (MEO + GEO + IGSO)
Symbol
n_BeiDou
Quantity
BeiDou satellites
Value
20,200 km
Symbol
h_GPS
Quantity
GPS orbital altitude
Value
19,100 km
Symbol
h_GLONASS
Quantity
GLONASS orbital altitude
Value
23,200 km
Symbol
h_Galileo
Quantity
Galileo orbital altitude
Section Title
GNSS Constellations: GPS, GLONASS, Galileo, BeiDou
Important Facts
- GPS: 24–30 active satellites; oldest GNSS; global coverage; frequencies L1 = 1575.42 MHz, L2 = 1227.60 MHz
- GLONASS: 24 satellites; Russian system; similar frequencies to GPS; useful redundancy, especially high latitudes
- Galileo: 30 satellites; European system; full constellation operational 2024; civilian codes on multiple frequencies
- BeiDou: 30+ satellites; Chinese system; strong Asia-Pacific coverage; best for Philippines in combination with GPS
- Multi-GNSS improves availability in urban/forest/canyon environments (satellite count increases, PDOP improves)
- Each constellation has different orbit geometry; combining them significantly speeds ambiguity fixing (10–100× faster)
- Code modulation varies by constellation (GPS C/A on L1, GLONASS C/A, Galileo E5b, BeiDou B1); receivers must support all
- Frequency diversity: Galileo and BeiDou have additional frequencies (E5a/E5b, B2a) → potential better iono correction
Key Definitions
Term
GPS (Global Positioning System / NAVSTAR)
Example
GPS alone provides 4–12 satellite visibility at any time; minimum 4 for 3-D fix
Definition
U.S. space-based GNSS constellation; 24–30 satellites in 6 orbital planes at ~20,200 km altitude; all-in-view within 5 min typical.
Term
GLONASS (Globalnaya Navigazionnaya Sputnikovaya Sistema)
Example
Combined GPS + GLONASS improves satellite availability in obstructed areas (urban canyons, forests)
Definition
Russian GNSS constellation; 24 satellites in 3 orbital planes at ~19,100 km; same dual-frequency architecture as GPS.
Term
Galileo (Galileo System)
Example
Full operational constellation as of 2024; improving accuracy and redundancy
Definition
European GNSS constellation; 30 satellites (24 active + 6 backup) at ~23,200 km; newer frequencies (E1, E5a, E5b, E6) with civilian access.
Term
BeiDou (BDS / Compass)
Example
Strongest coverage in Asia-Pacific region (Philippines included); improving rapid growth
Definition
Chinese GNSS constellation; 30+ satellites (MEO + GEO + IGSO orbits) at various altitudes; dual-frequency for civilians.
Term
Multi-GNSS / Multi-Constellation Receiver
Example
Modern survey receivers track all 4 constellations; fixes ambiguities 2–3× faster than GPS-only
Definition
Receiver tracking GPS + GLONASS + Galileo + BeiDou simultaneously; improves satellite count, geometry, and convergence speed.
Diagrams To Know
- Constellation orbital planes and satellite distribution (GPS, GLONASS, Galileo, BeiDou)
- Frequency bands comparison (GPS L1/L2 vs Galileo E1/E5 vs BeiDou B1/B2/B3)
- Global coverage map showing GPS vs multi-constellation satellite availability
Common Values
Value
1998
Symbol
yr_RA8560
Quantity
RA 8560 enactment year
Value
1965 (RA 4374)
Symbol
yr_PRS92
Quantity
PRS92 adoption year
Value
4 zones (Luzon, Visayas, Mindanao, Palawan with PCS)
Symbol
n_zones
Quantity
PPCS standard zones
Section Title
Philippine Legal & Regulatory Framework for GNSS
Important Facts
- All Philippine surveys must use PRS92 datum (not WGS84 directly); non-compliance violates RA 8560 and RA 4374
- GNSS raw results in WGS84 must be TRANSFORMED to PRS92 before legal/property use; document transformation method
- Licensed Geodetic Engineers required for cadastral surveys, boundary disputes, property deeds under RA 8560
- NAMRIA control monuments define PRS92 frame; all surveys must tie to nearest NAMRIA benchmark
- PRISM (Philippine Reference System CORS Network) provides real-time RTK corrections tied to PRS92; operational since ~2010
- PRS92 coordinates mandatory on all legal documents, property deeds, engineering designs, government maps
- Datum transformation validation: NAMRIA publishes official transformation grids (BX files) and 7-param Helmert constants
- Surveyors must document survey standards (RA 8560 compliance), datum used, transformation applied, and monument ties
Key Definitions
Term
RA 8560 (Geodetic Engineer License Law, 1998)
Example
Only licensed Geodetic Engineers (PRC certified) can conduct surveys for property deeds, cadastral records in Philippines
Definition
Philippine law defining professional qualification and scope of geodetic engineers; mandates PRS92 for all surveys; governs cadastral/property surveys.
Term
RA 4374 (PRS92 Adoption & Standardization, 1965)
Example
All Philippine government maps, coordinates, property records must use PRS92; non-compliance invalidates legal documents
Definition
Philippine law adopting Clarke 1866 ellipsoid and PRS92 datum as official reference system; established NAMRIA as official mapping agency.
Term
PD 1529 (Surveyors License Decree, 1978; repealed by RA 8560 but principles remain)
Example
Historical context for evolution of surveying profession in Philippines; RA 8560 supersedes
Definition
Historical decree on surveyor licensing; modern surveying (GNSS-based) regulated under RA 8560 instead.
Term
CA 141 (Commonwealth Act 141 / Public Land Act, 1936)
Example
Surveys under CA 141 must follow RA 8560 standards; GNSS surveys tied to PRS92 monuments
Definition
Philippine land ownership and cadastral survey law; defines free patents, homesteads, and survey requirements for public lands.
Term
NAMRIA (National Mapping and Resource Information Authority)
Example
NAMRIA publishes transformation parameters (PRS92 ↔ WGS84); maintains PRISM (PRS92-based RTN) for real-time GNSS
Definition
Philippine government agency maintaining official geodetic control network (PRS92 monuments), maps, and reference systems.
Term
PPCS (Philippine Plane Coordinate System)
Example
Survey blueprints, engineering designs, cadastral maps use PPCS coordinates (Easting, Northing in metres)
Definition
Projected (plane) coordinate system based on PRS92 and UTM projection (Transverse Mercator); coordinates in metres.
Diagrams To Know
- Philippine survey regulatory hierarchy: RA 8560 → RA 4374 → CA 141 → NAMRIA implementation
- NAMRIA control monument network map (Luzon, Visayas, Mindanao)
- PRISM RTK coverage map across Philippines
Must Remember
Item
4 SATELLITES MINIMUM for 3-D fix: 3 unknowns (X, Y, Z) + 1 unknown (receiver clock bias Δt_receiver) = 4 pseudorange equations required. Three satellites alone cannot solve a 3-D position.
Item
Pseudorange ρ = c × Δt where c = 299,792,458 m/s (exact). Always use correct value; off-by-one order of magnitude is a common exam trap.
Item
Carrier phase is PRECISE (~mm) but AMBIGUOUS; pseudorange is COARSE (~m) but UNAMBIGUOUS. RTK success depends on rapid ambiguity resolution (FIXED status).
Item
DOP multiplies measurement error: Accuracy ≈ DOP × σ_measurement. Lower DOP is BETTER. PDOP < 4 is excellent; > 16 is poor. DOP is geometric only (does not include atmospheric errors).
Item
DGPS (pseudorange differential) gives 0.5–1 m accuracy; RTK (carrier-phase differential with ambiguity fix) gives 2–5 cm. RTK requires FIXED integer status; FLOAT is similar to DGPS.
Item
WGS84 ≠ PRS92. All GNSS results from WGS84 MUST be transformed to PRS92 for Philippine legal use (RA 8560, RA 4374). Difference ~1 m; do NOT use informal shift.
Item
Multi-constellation (GPS + GLONASS + Galileo + BeiDou) improves satellite availability and speeds ambiguity fixing 2–10×. Modern receivers exploit this; single-constellation slower.
Item
Ionospheric delay is FREQUENCY-DEPENDENT (~40.3 × TEC / f²); Tropospheric delay is FREQUENCY-INDEPENDENT (~2.5 m zenith). Dual-frequency removes iono; both remain in single-frequency.
Item
Static survey post-processing accuracy: 5 mm + 1 ppm of baseline (dual-frequency, good conditions). Faster than RTK for long baselines but requires offline processing and waiting for precise ephemeris.
Item
Time-to-fix (RTK ambiguity initialization) depends on baseline, geometry (DOP), satellite count, signal strength. Typical: 10–30 s dual-frequency; 1–5+ min single-frequency. Plan field sessions accordingly.
Last Minute Tips
Tip
Always write the 4 SATELLITES = 4 UNKNOWNS fact when asked 'why do you need 4 satellites?' Examiners test this fundamental concept constantly. Missing this loses easy marks.
Tip
When calculating pseudorange, remember c = 299,792,458 m/s (not 3×10⁸). Travel time Δt in SECONDS, not milliseconds. Check units: m/s × s = m. A 0.1 s error = ~30 million metres wrong; catch it.
Tip
DOP formula trap: Accuracy ≈ DOP × σ means if you double DOP, accuracy doubles (gets WORSE, not better). Low DOP = good. High DOP = bad. Invert in your head: smaller number = better precision.
Tip
On WGS84 vs PRS92 questions: ALWAYS state 'GNSS is WGS84, must transform to PRS92 for Philippines (RA 8560)' to show legal knowledge. Bonus marks for citing transformation method (7-param or grid).
Tip
RTK FIXED vs FLOAT distinction: if you see 'FIXED' you have cm accuracy; 'FLOAT' is still ~0.5–1 m (same as DGPS). Exam often asks 'why wait for FIXED if FLOAT is instant?' Answer: accuracy difference.
Comparison Tables
Rows
Values
- ~1 m (coarse)
- ~2–5 mm (precise)
Property
Precision
Values
- UNAMBIGUOUS (direct range)
- AMBIGUOUS (integer N unknown)
Property
Ambiguity
Values
- Fast (~1 s)
- Slow (minutes+ for fixing N)
Property
Speed of measurement
Values
- High (1–3 m error)
- Low (5–50 mm error)
Property
Multipath sensitivity
Values
- Navigation, DGPS, rapid positioning
- Precise geodetic surveys, RTK, control
Property
Typical use
Values
- NO (inherently unambiguous)
- YES (critical; time-consuming)
Property
Integer ambiguity resolution needed?
Values
- None
- YES; must detect & repair
Property
Cycle slip problem
Columns
- Characteristic
- Pseudorange (Code)
- Carrier Phase
Table Title
GNSS Observables: Pseudorange vs Carrier Phase
Rows
Values
- Real-time or post
- 0.5–1 m
- 1–2 min
- Navigation, rapid surveys, <50 km baseline
Property
DGPS (Pseudorange Diff)
Values
- Real-time (FIXED)
- 2–5 cm (FIXED); 0.5–1 m (FLOAT)
- 10 s–5 min
- Stake-out, machine guidance, 20–50 km baseline
Property
RTK (Carrier Phase Diff)
Values
- Real-time (unfixed)
- 0.5–1 m
- Immediate
- Same as DGPS; no benefit until fixed
Property
RTK (FLOAT, not fixed)
Values
- Post-processing (offline)
- 5 mm + 1 ppm baseline
- Hours–days
- Precise control surveys, long baselines 50+ km
Property
Static Post-Processing
Values
- Post-processing
- 1–2 cm + 1 ppm
- 10 min + post-proc
- Quick control densification, 5–20 km
Property
Rapid-Static
Columns
- Method
- Mode
- Accuracy
- Time-to-Result
- Best Use
Table Title
DGPS vs RTK vs Static Post-Processing
Rows
Values
- USA
- 24–30
- 20,200
- 6
- L1 (1575.42 MHz), L2 (1227.60 MHz)
- Global
Property
GPS
Values
- Russia
- 24
- 19,100
- 3
- L1 (1602+N×562.5 kHz), L2
- Global
Property
GLONASS
Values
- Europe
- 30
- 23,200
- 3
- E1, E5a, E5b, E6
- Global (full 2024)
Property
Galileo
Values
- China
- 30+
- Various (MEO/GEO/IGSO)
- Mixed
- B1, B2, B3
- Strong Asia-Pacific
Property
BeiDou
Columns
- Constellation
- Country
- Satellites
- Altitude (km)
- Orbital Planes
- Key Frequencies
- Coverage
Table Title
GNSS Constellations: GPS vs GLONASS vs Galileo vs BeiDou
Rows
Values
- Excellent
- ~5–10 m
- ~7–15 m
- Ideal (rare without augmentation)
Property
< 2
Values
- Good
- ~10–20 m
- ~15–30 m
- Recommended for surveys; good geometry
Property
2–4
Values
- Moderate
- ~20–40 m
- ~30–60 m
- Acceptable; caution on critical work
Property
4–8
Values
- Poor
- ~40–80 m
- ~60–120 m
- Avoid if possible; degraded solution
Property
8–16
Values
- Very Poor
- > 80 m
- > 120 m
- REJECT; do not use for surveys
Property
> 16
Columns
- PDOP Range
- Rating
- Horizontal Accuracy (σ = 5 m)
- Vertical Accuracy (σ = 5 m)
- Survey Suitability
Table Title
DOP Quality Ratings & Positioning Accuracy Impact
Rows
Values
- Earth's centre
- WGS84 (a=6378137 m)
- Geocentric, global
- Global (GPS)
- NOT acceptable for final legal/property surveys
Property
WGS84
Values
- Earth's centre (fixed 1992)
- Clarke 1866 (a=6378206.4 m)
- Local Philippine datum, frozen epoch
- Philippines
- MANDATORY for all Philippine surveys by law (RA 8560)
Property
PRS92
Values
- Earth's centre (continuously updated)
- GRS80 (nearly WGS84)
- Geocentric, high-precision global
- Global (geodetic community)
- Optional; more accurate than WGS84 but requires transformation to PRS92
Property
ITRF
Columns
- Frame
- Origin
- Ellipsoid
- Datum Type
- Use Region
- Philippine Legal Status
Table Title
WGS84 vs PRS92 vs ITRF Reference Frames
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