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Modern aviation uses a combination of conventional ground-based navaids (VOR, NDB, DME) and satellite-based systems (GPS/GNSS). Understanding each system's capabilities and limitations is essential for both VFR and IFR operations.

Heading, Track, and Bearing

Key Definitions

Term Definition Reference
True North (TN) Geographic North Pole direction Fixed, geographic reference
Magnetic North (MN) Direction of Earth's magnetic field Varies by location and time
True Heading (TH) Aircraft nose direction, referenced to True North Calculated from TC + or − WCA
Magnetic Heading (MH) Aircraft nose direction, referenced to Magnetic North TH ± magnetic variation
Compass Heading (CH) Reading on compass (affected by deviation) MH ± compass deviation
True Track (TT) Intended path over ground, referenced to True North Flight planning reference
Magnetic Track (MT) Intended path over ground, referenced to Magnetic North MH with zero wind
Ground Track Actual path flown over ground (wind corrected) ATC/radar reference

The conversion chain: True ➜ (±Variation) ➜ Magnetic ➜ (±Deviation) ➜ Compass. Mnemonic: "True Virgins Make Dull Company" (True Variation Magnetic Deviation Compass). West variations ADD, East SUBTRACT (WAEA) when converting True to Magnetic.

VOR (VHF Omnidirectional Range)

VOR is a ground-based radio navigation system operating in the VHF band (108–118 MHz). It provides magnetic bearing information to/from the station. VORs form the backbone of most instrument airways worldwide.

VOR Term Explanation
Radial A bearing FROM the VOR station (magnetic). Radial 090 points East from the station.
Course A bearing TO the VOR station = reciprocal of radial (radial − 180°)
CDI (Course Deviation Indicator) Needle showing whether aircraft is left/right of selected course
OBS (Omni Bearing Selector) Knob to select the desired course/radial
Full-scale deflection Typically ±10° from course for CDI (some instruments ±5°)
TO flag Aircraft is heading generally toward the station
FROM flag Aircraft is moving generally away from the station
Cone of Confusion Area directly overhead VOR where signal is unreliable (~30° cone)

VOR Types

Type Full Name Frequency Range
TVOR Terminal VOR 108–112 MHz 25 nm
BVOR Branch VOR 112–118 MHz 40 nm
HVOR High-altitude VOR 112–118 MHz 130+ nm (above FL180)
DVOR Doppler VOR 108–118 MHz Higher accuracy, resistant to terrain

NDB (Non-Directional Beacon)

NDB is a ground-based medium-frequency (190–1750 kHz) radio beacon. Unlike VOR, it transmits in all directions without providing bearing information directly — the aircraft's ADF (Automatic Direction Finder) receiver shows the direction to the station.

NDB Term Explanation
Bearing Direction to/from the NDB in degrees
Relative bearing Bearing to station relative to aircraft nose (0° = straight ahead)
QDM Magnetic heading to steer to reach the station (zero wind)
QDR Magnetic bearing from the station (radial equivalent)
ADF Automatic Direction Finder — cockpit instrument showing relative bearing to NDB
Magnetic bearing to station Magnetic heading + relative bearing (if <360°) else − 360°

NDB/ADF systems are subject to errors from: night effect (atmospheric distortion at night), coastal refraction (bending over coastlines), mountain effect, and thunderstorm interference (ADF may point toward electrical storms). Use with awareness of limitations.

DME (Distance Measuring Equipment)

DME provides slant range distance from an aircraft to a ground station. It works by the aircraft interrogating the ground station and measuring signal round-trip time. Usually co-located with VOR (VOR/DME) or ILS (ILS/DME).

  • Measures slant distance, not ground distance (difference negligible above ~30 nm or above ~3,000 ft AGL)
  • Frequency paired with VOR — selecting the VOR frequency automatically tunes DME
  • Readout: nautical miles
  • Can also display groundspeed and time to station
  • Multiple DMEs can be used for position fixing (DME/DME)

GPS / GNSS

Term Meaning
GNSS Global Navigation Satellite System (umbrella term)
GPS US system (24+ satellites), most common in aviation
GLONASS Russian system
Galileo European system
SBAS Satellite-Based Augmentation System (WAAS in USA, EGNOS in Europe) — improves accuracy to ~3 m
RNP Required Navigation Performance — performance-based nav with on-board monitoring and alerting
RNAV Area Navigation — enables routes not tied to ground-based navaids
LPV Localizer Performance with Vertical guidance — precision-like approaches using GPS + SBAS

GPS approaches include LNAV (lateral only), LP (lateral performance), LNAV/VNAV (lateral + baro-vertical), and LPV (lateral + SBAS vertical). LPV minimums can be equivalent to ILS CAT I. Always check current NOTAMs for GPS/SBAS outages before flight.

Dead Reckoning (DR)

Dead reckoning is the process of estimating current position based on a known previous position, heading, speed, and elapsed time — without reference to external fixes. Essential for situational awareness when primary navaids are unavailable.

DR Position Calculation: Known position: overhead VOR at 10:00Z True airspeed: 120 kt Wind: 270°/20 kt True heading: 090° Wind correction angle (WCA) ≈ arcsin(wind speed × sin(wind angle) / TAS) Ground speed ≈ TAS ± headwind/tailwind component After 30 minutes, estimated position = known position + (GS × 0.5 hours) along ground track
Calculation Formula Notes
Wind Correction Angle (WCA) WCA = arcsin(crosswind component / TAS) Use flight computer or calculator
Ground Speed GS = TAS ± headwind/tailwind + tailwind, − headwind
Time to fix Time = Distance ÷ Ground Speed In hours; ×60 for minutes
Distance Distance = GS × Time GS in knots, time in hours = nm
Fuel required Fuel = fuel flow × time Always add required reserves