Free-space optical (FSO) communication is experiencing strong growth, driven by the deployment of large-scale satellite constellations and the increasing use of optical inter-satellite links (OISL) across LEO, MEO, and GEO orbits. These systems depend on Optical Communication Terminals (OCTs) equipped with Fine/Fast Steering Mirrors (FSM) to mitigate platform disturbances such as jitter, pointing inaccuracies, and micro-vibrations, ensuring stable and precise optical links. At the same time, the New Space sector imposes strict requirements on size, weight, and power (SWaP), as well as on cost efficiency, manufacturability, and scalability, particularly as constellation programs demand production volumes reaching tens of thousands of units.
To address these constraints, CEDRAT TECHNOLOGIES has developed the CONECS project, aimed at designing space-qualified piezoelectric FSMs and their associated drive electronics tailored for LEO constellation applications. Building on significant in-flight heritage, this work has led to a new generation of FSMs combining high pointing accuracy, robustness against launch and space environments, and compatibility with large-scale manufacturing.
The P-FSM35XS, based on the DTT35XS architecture previously validated in missions such as PHARAO and PAM30, has been specifically enhanced for New Space use cases. The redesigned system delivers a 27% increase in angular range, achieving up to 6.1 mrad, while preserving bandwidth levels required for FSO stabilization. Key improvements include a simplified half-bridge strain-gauge measurement scheme, integrated offset correction within the mechanism, reduced cabling complexity, and design optimizations that facilitate manufacturing and improve reliability, as well as interchangeability at system level.
For applications requiring larger deflection angles, the P-FSM150S offers mechanical strokes up to 18 mrad, enabled by newly developed amplified piezoelectric actuators (APA150S). Its flexible mirror interface supports both high-reliability silicon carbide (SiC) mirrors mounted with screws and more cost-effective fused silica (SiO₂) mirrors for COTS-oriented New Space solutions. Qualification and lifetime testing demonstrate positioning resolutions below 20 µrad, resonance frequencies exceeding 700 Hz, resistance to launch loads, and operational lifetimes beyond 10⁹ cycles. Optical bench validation further confirms improved beam stabilization and pointing performance.
Control of these mechanisms is ensured by the CCBu20-NS dual-channel piezo controller, which integrates push-pull actuation, strain-gauge signal conditioning, digital closed-loop PID control with adjustable notch filtering, as well as telemetry and telecommand capabilities. The controller achieves closed-loop bandwidths above 250 Hz and withstands radiation levels up to 30 krad, making it well suited for LEO New Space missions.
Altogether, these developments form a consistent, scalable, and cost-efficient FSM product line from CEDRAT TECHNOLOGIES, designed to meet the stringent pointing and stabilization requirements of SmallSat optical communication constellations.
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