A spacecraft that finds itself.

Two identical open-source CubeSats built by students at Carnegie Mellon and Instituto Superior Técnico, designed to tackle the lost-in-space problem for small spacecraft.

The problem

Lost in space

Small spacecraft often depend on GNSS or ground tracking to know where they are. But GNSS adds cost, power, and integration complexity, while ground tracking depends on external infrastructure and operations.

Argus asks a different question: what if a CubeSat could recover its orbit and attitude by looking at Earth?

The payload

Argus captures Earth images onboard.

The spacecraft uses visual observations of Earth to generate landmark bearing measurements.

  • 01Earth image
  • 02Region classification
  • 03Landmark detection
  • 04Bearing measurement
Stylized Earth frame captured from orbit
region · RCNet
L1L2L3
ARGUS

The payload turns images into geometry.

A region classifier narrows down where the spacecraft is looking. A landmark detector finds visual features. Those detections become bearing measurements that can be used for orbit and attitude estimation.

  1. 1

    Earth image

    Raw frame captured onboard

  2. 2

    Region classification

    RCNet narrows the view to a salient region

  3. 3

    Landmark detection

    LDNet pinpoints ground features

  4. 4

    Bearing vectors

    Detections become spacecraft-to-landmark bearings

  5. 5

    Measurement packet

    Geometry ready for the estimator

Sensor fusion

Argus combines what it sees with what it feels.

Landmark bearings from onboard images are fused with inertial measurements through a batch nonlinear least squares estimator to recover orbit and attitude.

Validation

A GNSS receiver flies only as the truth reference.

Argus compares its vision-based solution against onboard GNSS to evaluate estimation accuracy in orbit.

  • GNSS reference
  • Argus visual estimate

residual ↓ converging

The fleet

Two identical Arguses. One open mission architecture.

Flying two spacecraft gives the mission more opportunities for data collection, validation, operations practice, and community engagement.

Two more experiments ride along.

Doppler-based ground OD

Ground stations receive GMSK signals and study how SNR, bandwidth, and duty cycle affect orbit determination precision.

Amateur radio packet repeater

Argus will support an amateur packet repeater as operational constraints allow.

Every gram engineered in-house.

Scroll to open the spacecraft.

The build

Built in-house, end to end.

Electronics, flight software, payload, communications, integration, and operations are developed by the Argus team using commercial off-the-shelf components wherever possible.

flight unit open on the bench
flight unit open on the bench
power testing, both units
power testing, both units
stowed in the deployer pod
stowed in the deployer pod
deployment test
deployment test
ready for integration
ready for integration

Follow Argus from lab bench to low Earth orbit.