ADCS & Navigation — Space Hardware Marketplace

ARGO 1.0 Star Tracker

• InterfaceRS422, SpaceWire, CANBus (redundant)
• Flight heritageIn-orbit demonstration on D-Orbit ION SCV2, launched Jan 2021, validated through Jul 2022
• TRL8 (flight-demonstrated)

Flight-proven multicamera autonomous attitude determination system (star tracker) for small satellites.

READY ADCS

• Designed forSmall satellites and CubeSats
• Orbit compatibilityAll LEO orbits
• ConfigurationsREADY-200, READY-100, READY-16U, READY-6U

Indra's READY ADCS is a turnkey attitude determination and control system for small satellites and CubeSats, designed for…

Navishield Anti-Jam / Anti-Spoofing GNSS Antenna

• Protected signalsGalileo PRS, Galileo OS, GPS
• FunctionAnti-jam / anti-spoofing CRPA antenna
• Related receiverG3Star multi-constellation receiver (supports Galileo HAS)

Next-generation CRPA antenna system protecting GNSS receivers against interference and spoofing.

READY ADCS (READY-6U / 16U / 100 / 200)

• Product familyREADY-6U, READY-16U, READY-100, READY-200
• Target platform classCubeSats (6U/16U) through 100-200 kg smallsat buses
• Orbit regimeLEO

Turnkey attitude determination and control system family for CubeSats and small satellites in LEO.

MACM Attitude Control Magnetometer

Compact tri-axial fluxgate magnetometer for LEO satellite attitude determination, 249 g, 28 V RS485 interface.

ARIETIS

ARIETIS is an ITAR-free, space-qualified, rad-hard 3-axis gyroscope designed for use as a primary gyro or coarse rate…

Earth Horizon Sensor

The Pyxis Space Earth Horizon Sensor provides nadir-vector measurement for CubeSat attitude control using both visible (VIS) and…

Reaction Wheel

The Pyxis Space Reaction Wheel is a miniaturized momentum exchange device for precise attitude control of CubeSat and…

LN-200S Inertial Measurement Unit

Fiber-optic inertial measurement unit for space applications with flight heritage on Mars rovers and deep-space probes.

Redwire Coarse Sun Sensor – Cosine Type

Small, lightweight single-detector sun sensor with cosine-symmetric field of view for solar-array pointing and sun acquisition.

Redwire Coarse Sun Sensor – Pyramid

2-axis, 4-detector pyramid-configuration coarse sun sensor for solar array pointing and sun acquisition.

AAC Clyde Space RW210 Reaction Wheel

Low mass, low power CubeSat reaction wheel with fire-and-forget speed/torque control, available in 1.5, 3.0, or 6.0 mN.m.s…

NanoSense M315

The NanoSense M315 is a flight-proven, compact, and low-noise magnetometer with an I2C interface, designed for nanosatellites requiring…

NanoTorque GSW-600

The NanoTorque GSW-600 is a compact, high-performance reaction wheel system consisting of four wheels in a pyramid setup,…

AOCS & GNC Sensors

• Astrix 200 bias stability<0.0005°/h
• Astrix 120 bias stability<0.01°/h, startup <3s
• Interfaces1553B, RS422

Airbus offers a comprehensive range of avionics sensors for precise attitude control and navigation in space, including Astrix…

ASTRIX 1090 Inertial Measurement / Accelerometer Unit

• Angular random walk<0.005°/√h
• Bias stability<0.01°/h
• ConfigurationOptional accelerometer channels for full inertial navigation

Three-axis fibre-optic inertial unit from the ASTRIX 1000 series offering low angular random walk and optional accelerometer channels…

Control Moment Gyroscopes (CMG 15-45S / 40-60S / 75-75S)

A range of compact, high-torque Control Moment Gyroscopes from Airbus for precise and agile satellite attitude control, covering…

AOCS/GNC Sensors

• Astrix bias stabilityas low as 0.0005°/h
• Astrix mission lifetimeexceeding 15 years
• Bass field of view±90°

A range of Airbus attitude and orbit control sensors comprising Astrix fibre-optic gyroscopes, Jena-Optronik star sensors, and BASS…