← ALL AVIONICS
GENERAL DYNAMICS / L3HARRIS

GPS III Receiver

Navigation ReceiverGNSS Receiver● Active
MASS
1.5 kg
POWER
15 W
REDUNDANCY
Dual-channel
RAD HARDENED
Yes
FIRST USE
Dec 2018

GPS III Receiver is a navigation receiver system manufactured by General Dynamics / L3Harris. It features dual-channel redundancy. Radiation hardened for space environments.

ABOUT GPS III RECEIVER

A GPS III receiver is a small electronics box on a rocket or spacecraft that listens to GPS satellites and works out, moment by moment, exactly where the vehicle is, how fast it is moving, and what time it is. It is the same idea as the GPS in a phone, but built tough enough to keep working through the violent ride into space.

Quick facts

  • What it is: an onboard navigation and tracking sensor — not a satellite, but the receiver that picks up satellite signals.
  • Signals it uses: the U.S. GPS constellation, including modern GPS Block III/IIIF satellites and their encrypted military M-Code signals.
  • Typical design: a roughly 50-channel digital receiver built to navigate in high-dynamic, high-altitude conditions.
  • Antennas: usually two, mounted on opposite sides of the airframe so coverage holds as the vehicle rolls.
  • Output: position, velocity, and timing data (often shortened to PVT).
  • Secure variant: L3Harris’s Protected GPS-Mini (PGPS-M), an M-Code L1/L2 unit with a 10 Hz update rate and continuous atmospheric correction.

What it is and how it works

GPS satellites broadcast faint microwave signals on radio frequencies named L1 and L2 (modern units also receive the encrypted military signal called M-Code). The receiver’s antennas capture these signals, and by measuring the tiny time delays from several satellites at once — called pseudo-ranges — it solves for the vehicle’s three-dimensional position, velocity, and precise time.

The hard part on a rocket is what engineers call “high dynamics.” During ascent the vehicle accelerates and shakes violently and climbs through and above the altitude where most GPS users sit, so the receiver’s tracking loops — the circuits that stay locked onto each signal — are specially tuned to hold on. A spinning rocket body would otherwise lose line-of-sight to some satellites, which is why two antennas sit on opposite sides of the stage. Think of it like keeping two ears on opposite sides of your head so you never fully lose a sound as you turn.

The resulting PVT stream is put to work in three ways. First, it can be sent to the ground to replace radar tracking — a role called GPS Metric Tracking. Second, it can feed an automated flight safety system that can end the flight if the vehicle strays. Third, it can be blended with an inertial measurement unit (an IMU, a sensor that feels motion using gyroscopes and accelerometers) inside a Kalman filter — a math routine that fuses sensors — to produce the navigation answer the flight computer uses to steer.

Why it matters

Precise, continuous knowledge of where a rocket is underpins both safety and accuracy. As a GPS Metric Tracking source, the receiver lets ranges retire expensive, location-limited ground radars, and it is a key enabler of Autonomous/Automated Flight Safety Systems that can destroy an off-course vehicle without a human in the loop. That, in turn, allows higher launch cadence and launches from sites without full radar coverage.

As a navigation sensor, it gives the guidance system an absolute position fix that bounds the slow drift of inertial navigation, improving orbital-insertion accuracy and enabling autonomous rendezvous and docking. The shift to M-Code GPS III signals, through receivers like PGPS-M, hardens the system against jamming and spoofing — which is why the U.S. National Security Space Launch program requires it under its “Assured Access to Space” initiative.

A note on the name

“GPS III” can mean two different things. GPS Block III/IIIF are the newest GPS satellites (built by Lockheed Martin with an L3Harris navigation payload) that broadcast the signals. A GPS III receiver is the onboard box on a rocket or spacecraft that receives them. The satellites are the source; the receiver is the user on the vehicle.

Where it is used and notable examples

  • Atlas V (United Launch Alliance): flew the GPS Metric Tracking receiver on certification flights in 2012 — first from Cape Canaveral in February, then from Vandenberg in September — demonstrating GPS-based tracking as a replacement for ground radar.
  • Delta IV (ULA): completed a GPS Metric Tracking certification flight from Cape Canaveral in October 2012.
  • Falcon 9 (SpaceX): carries onboard GPS as part of its navigation, supporting GPS-aided tracking and its autonomous flight safety approach.
  • L3Harris PGPS-M: an embedded M-Code L1/L2 receiver used on launch vehicles and missiles for range tracking, navigation aiding, and as an external sensor for autonomous flight safety units.
  • NASA Orion: uses a single-frequency (L1) GPS receiver alongside two IMUs and barometric altimeters, fused in an extended Kalman filter, for near-Earth navigation.

One limit is worth knowing: GPS coverage effectively ends above the constellation’s altitude, so it is unreliable in high Earth orbit and at the Moon. Deep-space and lunar vehicles instead rely on inertial navigation, star trackers, optical navigation, and ground tracking — which is why a GPS receiver is almost always paired with an IMU rather than used alone.

OPERATING PRINCIPLE

Multi-frequency GNSS reception (L1/L2/L5) with anti-jam capability and high-dynamic tracking loops

VEHICLES USING THIS SYSTEM
Various launch vehiclesISSGPS III constellation
SPECIFICATIONS
CATEGORYNavigation Receiver
TYPEGNSS Receiver
MANUFACTURERGeneral Dynamics / L3Harris
MASS1.5 kg
POWER CONSUMPTION15 W
REDUNDANCYDual-channel
RADIATION HARDENEDYes
ACCURACY< 1 m CEP with dual frequency
FIRST USEDecember 23, 2018
STATUSActive
DETAILED SPECS
SIGNALSL1/L2/L5
CHANNELS24
DYNAMICS> 15 g
TTFF< 60 s

Related Articles