HARDWARE / PRODUCTAdded 13 Jul 2026

ASTROgyro Integrated Attitude Determination System

Jena-Optronik

Integrated star tracker + gyro AOCS unit: 2x ASTRO APS star sensors + Coriolis Vibratory Gyroscopes IRU, 30 Hz output, <1/<8 arcsec star tracker accuracy, <0.005 deg/sqrt(hr) gyro ARW, TRL 9 (SES-20/21).

Typed specifications2 values

Discloses 1 of 12 fields engineers filter by in this category (category median 8).

Envelope (L×W×H)
~230 x 230 x 170 mm
product page
Update rate
30 Hz
product page

Each value is typed with its unit and measurement condition and cites the datasheet page it was taken from. Nothing is guessed: a field that is absent here has not been published by the manufacturer. machine-extracted ✓ checked by NewSpace Market ✓ manufacturer confirmed by the manufacturer.

As published by the supplier16 lines, in the manufacturer's own wording
Configuration
2x AGS (star sensor) + 1x AGI (Inertial Reference Unit)
System update rate
30 Hz
Ags bias error
<5 arcsec (full temp range)
Ags noise equivalent angle xy (1-sigma)
<1 arcsec
Ags noise equivalent angle z (1-sigma)
<8 arcsec
Ags mass (each)
~2 kg
Agi full scale range
+/-20 deg/s (coarse); +/-1 deg/s (fine)
Agi angle random walk
<0.005 deg/sqrt(hr) per axis
Agi bias instability (1-sigma)
<0.05 deg/hr per axis
Agi noise equivalent rate
<2 deg/hr rms (0.1-15 Hz)
Agi mass
~7.8 kg
Agi dimensions
~230 x 230 x 170 mm
Power (cold-redundant)
<21 W nominal (1x AGS + 1x AGI)
Power (hot-redundant)
<54 W nominal (2x AGS + 1x AGI)
Interface
MIL-STD-1553B, 28 V power
TRL
9 (flight heritage on SES-20 and SES-21)

About

The Jena-Optronik ASTROgyro is an integrated attitude determination system combining ASTRO APS star trackers (AGS units) with Coriolis Vibratory Gyroscopes in an Inertial Reference Unit (AGI). The system provides full 3-axis attitude measurement with superior performance during high slew rates and bridging during star tracker outages. Standard configuration is two AGS star sensors plus one AGI IRU in a cross-strapped hot- or cold-redundant arrangement. The AGI IRU provides 30 Hz attitude rate output with less than 0.005 deg/sqrt(hr) angle random walk and less than 0.05 deg/hr bias instability. Full ITAR-free design available. First flight on SES-20 and SES-21 geostationary satellites, TRL 9.

Documentation

No public datasheet yet — request the datasheet / ICD from the supplier.

Source: www.jena-optronik.de ↗

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