GI-CVG-A23XXD A-Series 3-Axis CVG Digital Gyroscope
Innalabs3-axis Coriolis Vibratory Gyroscope with RS422 digital output, 0.3°/hr bias stability, 500K+ hr MTBF.
449 satellite platforms, components and ground equipment from manufacturers worldwide.
3-axis Coriolis Vibratory Gyroscope with RS422 digital output, 0.3°/hr bias stability, 500K+ hr MTBF.
RANGE is a mission consisting of two 1.5U CubeSats designed to demonstrate improved absolute orbital position knowledge and…
Star sensor technology for spacecraft attitude determination by XIOPM LSOT.
The Theseus Micro VPS (Visual Positioning System) is a plug-and-play GPS-denied navigation module for Group 1 drones and…
Indian company developing flywheel-based momentum and energy storage systems for satellite attitude control applications.
Chinese BeiDou navigation satellite system receiver manufacturer, producing GNSS chips and receivers for satellite and terrestrial applications.
Software-Defined Radio GNSS receiver with sub-0.5m position accuracy and Real-Time Precise Onboard Orbit Determination, selected for LeoStella LS-300…
Compact tactical-grade MEMS gyroscope module with 0.3 deg/hr bias stability, LEO-proven on over 30 satellite programs since 2012.
Hydra is a high-performance, modular star tracker system available in various configurations to match different mission profiles and…
Space-grade hemispherical resonator gyroscope (HRG) inertial reference unit for satellite navigation and attitude control.
Compact, high-accuracy star tracker for satellite attitude determination, flight-proven on over 50 missions worldwide.
The Nano Sun Sensor on a Chip (NanoSSOC) is a two-axis, low-cost sun sensor known for high accuracy…
The Advanced Coarse Sun Sensor (ACSS) is a highly reliable and radiation-hardened device for sun-tracking and attitude determination…
Miniature, fully autonomous digital sun sensor with <0.02° precision and CubeSat Space Protocol over I2C.
Fine-pointing CubeSat reaction wheels with BLDC motor, integrated IMU, and CubeSat Space Protocol support, for 1U-6U platforms.
Next-generation ADCS for 6U-16U CubeSats with star tracker and ±50 arcsecond pointing accuracy.
Fully integrated ADCS for 1U-3U CubeSats with 3 reaction wheels, magnetorquers, sun sensors, magnetometers, and gyroscopes.
GPS-denied autonomous navigation technology for UAVs and robotic platforms.
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