The AOCS and Pointing Systems test facilities, managed by the AOCS and Pointing Systems section supports R&D activities related to AOCS verification, AOCS prototyping, implementation of innovative techniques for AOCS design and tuning, high accuracy pointing and dynamic systems.
The AOCS verification facilities include the capability to test full CubeSats or AOCS breadboards on a 3-axis air bearing table. By careful mass balancing, it is possible to reproduce the low-disturbance orientation dynamics of space and physically stimulate sensors using a Sun lamp, magnetic field generator and an albedo straylight lamp. This allows the spacecraft AOCS to react as if it was on orbit such that its open or closed-loop behaviour can be witnessed in real-time. This test-as-you-fly facility is housed in an ISO8 clean tent, enabling ESA collaborators to gain extra confidence in their AOCS before flight. For instance, the customers can watch their AOCS perform detumble control and 3-axis slews.
The Pointing systems facilities are used to develop and tests a system mitigating the micro-vibrations generated by a wheel or by a cryo-cooler. This closed loop system uses force cells or IMU as sensors, a MICROLABBOX or a Raspberry PI as CPU, and 6x Proof Mass Actuators. Additionally, a fast and high definition camera and associated software performs motion amplification visualising and measuring micro-vibrations of complete structures in a non-intrusive way up to 3000Hz.
Piezo tip-tilt mirror and associated electronics from PI
S330, S335
IO hardware interface and software from dSpace
MICROLABBOX
Accelerometers and conditioners from PCB
352C33 (x2), 356B18 (x2)
ICP accelerometers from WILCOXON
731-207
Accelerometers conditioners from PCB
482C05
Laser Autocollimator from LDS
CONEX LDS
Fast Steering Mirror from CEDRAT
4-channel charge amplifier from BRUEL & KJAER
NEXUS 2692 (x3)
Optical table from NEWPORT
M-INT1-49-8-A
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