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1INTRODUCTIONIn nowadays data-driven society, Free Space Optical Communication, FSOC, is gaining momentum worldwide, considering the radio-technology limited bandwidth bottleneck. The market for a widespread exploitation of FSOC requires 24/7 operability of reliable optical channels. The ALASCA project (Advanced LGS AO for Satellite Communication Assessment) aims to prove the effectiveness of 24/7 optical feeder links with Laser Guide Star Adaptive Optics to solve the Point Ahead problem, towards ground to space optical communication. Establishing reliable optical channels between an Optical Ground Station and a satellite offers challenges mainly due to turbulence in the Earth’s atmosphere affecting the transmission through the atmosphere itself, especially during daytime conditions; and to the motion of the satellite, inducing an angular split, the Point Ahead Angle (PAA), between the beams transmitted (uplink) and received from the satellite (downlink), thus limiting the reliable compensation of the uplink signal based on the downlink signal. The use of Laser Guide Star Adaptive Optics technologies, so far developed in the astronomical and defence communities, is potentially an optimal solution for uplink wave-front measurements and pre-compensation of the feeder-uplink beam. As the typical PAA becomes critical in harsh turbulence conditions, an LGS-AO system would represent an enabling technology for the 24/7 operation of the free-space optical communication ground station, in order to reliably cope with the variability of the seeing conditions. The existing technology, developed so far for astronomical observatories, has to be adopted and adapted to the OFL space communication application. This paper describes the test facility infrastructure, its modular approach, its status, with a particular focus on the methods followed to solve the main issues posed by free space optical communications. 2ALASCA PROJECT OVERVIEW2.1Project outlinesThe ALASCA project is targeted towards the development of a reliable optical communication uplink from an optical ground station (OGS) to communication satellites. The project aims towards the creation of a full-fledged, TRL6 operational Optical Feeder Link (OFL) test facility at ESA OGS in Tenerife targeting 24/7 operability, based on the Laser Guide Star Adaptive Optics (LGS-AO), to solve the point-ahead problem on ground for space laser communications. The system uses CaNaPy system as a backbone [1]. CaNaPy is an LGS AO facility designed for night-time operation on astronomical targets, with a 50 W 589 nm laser. CaNaPy is developed by ESO with the support of INAF, Durham University, MPBC for the Raman amplifier and TOPTICA Projects for the laser chirping. ALASCA will upgrade the hardware and software of the CaNaPy facility to be suitable for ground-satellite optical communication development, upgrading the control electronics, control software and adding new subsystems for infrared optical feeder links, properly extending SatComm operation to harsh turbulence conditions, including daytime operation, with fast, predictive adaptive optics loop mode. The primary objective of ALASCA is, thus, to demonstrate how to remove atmospheric effects that prevent reaching the highest communication rates. The compensation of the atmospheric disturbance is furthermore affected by the Point Ahead Angle problem caused by the satellite motion, that is field anisoplanatism, and by the needed increase in AO loop speed due to the fast tracking for e.g. LEO satellites. LGS-AO application to OFL for correcting the uplink wavefront distortion induced by the turbulence in the atmosphere may become one fundamental technology for free space optical communication, as it strengthens and stabilizes the uplink communication signals received at the satellites, allowing an effective uplink pre-compensation, mitigating the effect of the point-ahead-angle; this will represent a milestone in guaranteeing a reliable optical channel ensuring 24/7 operations. Highlights:
2.2ALASCA teamThe project team, see Figure 3 for details, is led by Microgate and involves the participants listed herein:
The team combines some of the most experienced teams from LGS-AO in Europe, together with industrial teams specializing in adaptive optics and lasers. The group has been proficiently delivering projects together since 2000. 2.3Project planThe ALASCA project will deliver the first set of reliable Optical feeder Link (OFL) tests within 2 years from project kick off; in the third year it will deliver the complete 24/7 operation test. In particular, the project activities foresee a first part mainly focused on the design activities of the system, its preliminary test and integration. Once this phase is completed, the system is shipped to Tenerife at the ESA OGS, for the integration, commissioning and test activities in situ. 3ALASCA SYSTEM OVERVIEW3.1System outlineThe ALASCA system is designed to allow OFL test with LGS-AO system and uplink pre-compensation, in night- and day-time configurations, by an exchange of the interfaces, one for each configuration, with the OGS. The architectural concept block diagram is shown in Figure 5. The system’s main features are listed below:
3.2The 589 nm laserThe 589 nm laser utilizes the same narrow band, high power Raman Fiber Amplifier (RFA) technology as developed and patented by ESO in 2009 [6], engineered and optimized by MPBC to produce, in consortium with Toptica as main ESO contractor, the 22 W CW “Guide Star Laser”, installed since 2015 at the VLT Paranal Observatory and nowadays deployed at a good number of large observatories worldwide. Thanks to the MPBC novel development of a 100W CW RFA, the ESO CaNaPy laser could demonstrate 75 W CW of laser output power at 589nm, exceeding the original specification of 50W CW while keeping the same optical beam and functional properties as the commercial 22 W CW 589nm Toptica-MPBC lasers [5]. We must stress that to reach daytime operation (i.e. with harsh seeing conditions) in ALASCA the 75W power level is mandatory. Two specific features are being further developed by Toptica Projects and added to the CaNaPy 75W laser, to suit the needs of ALASCA:
3.3Atmospheric Monitoring UnitThe ALASCA facility aims at demonstrating a reliable 24/7 Free-Space Optical communication link between satellite and OGS; to that aim, atmospheric turbulence monitoring and forecasting plays a key role in optimizing the LGS-AO control and tests. Lumi Space and Durham University are developing an atmospheric monitoring system to characterize the Earth’s atmospheric turbulence during day and night. The instrument is called a Shack-Hartmann Image Motion Monitor (SHIMM). Figure 7 and Figure 8 show a photograph of the set-up and instrument, respectively. The instrument contains a Shack-Hartmann wavefront sensor to measure local wavefront tilt gradients in a grid of sub-apertures over a small (approximately 30 cm) telescope. The intensity variance (scintillation) in each sub-aperture is also measured. These two sources of data allow concurrent measurement of the turbulence parameters r0 (Fried parameter, describing overall turbulence strength) and θ0 (isoplanatic angle, describing turbulence angular correlation). The instrument will observe a single bright star close to zenith to minimise the potential effects of strong turbulence, a regime in which the instrument can no longer measure turbulence parameters. For more details, refer to [3]. 3.4OFL IR ModuleTwo optomechanical modules, one for the Tx of the OFL uplink laser and one for the Rx downlink GEO satellite signal are being developed by the consortium. A downlink fast tip-tilt mirror and an uplink fast beam steering mirror to compensate atmospheric induced jitter is included as part of the modules. The receiver section has an IR Pyramid WFS to be used either standalone, for AO without LGS, or as tip-tilt sensor for LGS-AO, using in both cases the satellite downlink laser signal as reference. The baseline operation wavelength is 1064nm, with provisions for 1550 nm. 3.5ALASCA Control System OverviewThe Instrument Control Software (ICS), the Real Time Control (RTC) and Microgate Control Electronics are the three main components of the ALASCA control system, as per Figure 9. The control software is split in two sections, the fast control (Real Time Control Software) and the slower instrumentation control (Instrument Control Software).
4PROJECT STATUS AND NEXT STEPS4.1Projects tradeoffs and specific technical solutions4.1.1Wavefront Sensor ChoiceWe have evaluated in simulation the LGS-AO closed loop performance considering a monostatic configuration. As shown in Figure 13 below, the monostatic design (same pupil for Tx-Rx) has several advantages w.r.t. the bistatic one (offset launch and receiver pupils), because it eliminates the cone effect and the uplink propagates along the same path of the downlink; conversely, the monostatic scheme poses some challenges due to the synchronization and scattering problems. The Pyramid WFS, like the curvature and shearing WFS, benefits from the full aperture advantage, i.e. it increases its sensitivity and performance when the reference source becomes smaller. In comparison with an equivalent Shack-Hartmann WFS (SH-WFS) system, the Py-WFS performance is superior whenever the reference source size is smaller than the diffraction limit of the Shack-Hartmann subapertures. Hence, considering a 1 m telescope diameter like the ESA OGS, a 10x10 subapertures Shack-Hartmann, operating at 589 nm, the Py-WFS starts showing better performances than the SH-WFS for LGS FWHM < 1.2 arcsec. In monostatic propagation with uplink correction, the simulations predict LGS FWHM of the order of 0.13 arcsec, hence there is considerable optical gain when using a Py-WFS with respect to the classical SH-WFS. The small LGS FWHM has implication in the Py-WFS modulation scheme during operation. Non linearities in the Py-WFS may be taken care by the Soft-RTC software, adjusting the system modal gains based on the actual averaged LGS FWHM when necessary. Also, automatic modal control contributes to the optimization of loop performances. 4.1.2Double AxiconFor the use of the 1.016 m full OGS telescope aperture, to avoid the uplink laser gaussian beams losses due to the vignetting of the secondary mirror (0.35 obstruction ratio), a double Axicon is introduced in the optical beam. It transforms the laser Gaussian beam intensity distribution into a Laguerre-Gauss annular distribution on the primary mirror (see Figure 14), without changing the beam collimation. A comparison between the LGS PSF seen at 90 km, for the cases of centrally obscured Gaussian Beam, top-hat ring intensity distribution at the OGS primary mirror, and Axicon Laguerre-Gauss ring intensity distribution is shown in Figure 14 on the right. The curves are normalized to the same total intensity. 4.2SimulationsNumerical simulations developed in the frame of the project aim at the quantification of the effect of the LGS-AO on the OFL performance. In particular, they are based on PASSATA, a proven end-to-end IDL-based code to simulate the monostatic, uplink pre-compensated LGS-AO loop with Pyramid WFS, as used in ALASCA, including physical Optics angular spectrum propagators for the OFL, developed by INAF [7]. PASSATA copes with the vertical distribution of the mesospheric sodium atoms emission, with the uplink pre-compensation and the time delays of the laser up-down links. Durham University has developed a E2E Monte-Carlo modelling tool coded in Python, with angular spectrum physical optics propagation functionality, simulating the AO-loop with a SH-WFS. As the physical Optics propagation has been developed in PASSATA in a second time, at the beginning of the project it was decided to carry out also a hybrid simulation: SOAPY physical propagation module will utilize, as inputs at each step, the atmospheric phase screens and the actuate DM at the telescope pupil conjugate, as obtained by PASSATA. This model is now used as a cross-check of the results obtained implementing the physical propagation in PASSATA, showing a good match. For parametric, quick analysis the ALASCA consortium uses the Durham University FAST code, which is using analytical expressions for evaluating the error terms of the AO loop, rather than numerical End2End simulations. See Figure 15 for details. 4.2.1Adopted Turbulent Atmosphere ModelFor the numerical simulations on the LGS-AO loop, we have used the mean night atmosphere from measurement campaigns done at Observatorio del Teide (OT) in Tenerife, the location of the ESA OGS telescope. 4.2.2Simulation of LGS-AO loop ControlWe have used the measured influence functions of the ALPAO 97-15 Deformable Mirror (DM) to establish the modal command matrix based on Karhunen-Loève modes. Modal gain optimization control and a simple integrator term have been used in the LGS-AO simulations. Noise terms such as photon noise, dark background, readout noise of the sensors and aliasing, as well as two-steps latency, have been taken into account. The Py-WFS has been considered adopting the following parameters; notice that no beam modulation is needed, at least for the seeing conditions used in the simulation. Table 1.Main Py-WFS parameters
4.2.3Simulation preliminary results: satellite uplink signal fluctuationsThe OFL 1075 nm laser is propagated concurrently with the LGS 589 nm laser, and pre-compensated in the uplink propagation by the DM of the LGS-AO loop. The LGS has a point ahead angle of 4.0 arcsec. The tip-tilt signal is derived from the downlink Alphasat signal, with the OGS telescope pointing at ALT 36 deg. The numerical simulations include the effects of air mass and anisoplanatism. The comparative simulations have been done using the hybrid model with Passata and Durham University SOAPY (indicated as Passata(phys) in the legend), and the Durham FAST semi-analytical code. In addition, the geometrical propagation obtained with Passata without physical propagation has been reported for reference. The end-to-end simulation with Passata embedding the physical propagation is ongoing, showing good agreement. The merit parameter is the distribution of received instantaneous power at the GEO satellite Alphasat, with its 15 cm diameter receiver: the signal fluctuation shall be kept within 10 dB while maximizing the power received. We can notice the importance of considering the physical optics propagation in particular with the 0.30 m pupil, since the scintillation log-amplitude variations in the final signal are more apparent due to the smaller launch aperture. We present Probability density results for the ALASCA nighttime (1.016 m OGS pupil) and daytime (30 cm pupil as subaperture of OGS). More results and cases obtained with three different simulation end-to-end models will be published in a coming paper. The large aperture propagation gives a higher signal concentration, with diffraction limited performance. The tip-tilt anisokinetism due to the angular distance between the satellite and the point-ahead LGS causes a residual uncorrected tilt which creates higher variability on the smaller OFL spot at the satellite, hence higher spread in the photometric probability density. The results for the 1.016 m pupil case could be dramatically improved if tip-tilt could be inferred from the LGS itself (not shown here). Other methods to slightly blur the OFL spot at the satellite would work as well, and are under investigation. The simulations will be extended to more atmospheric condition cases and anchored to real data once the ALASCA facility is in operation. 4.2.4LGS-AO loop Results: Monostatic vs BistaticThe following table summarizes the long exposure performances of the LGS-AO loop, for the cases of 1 kHz and 2 kHz operation, with seeing of 0.7 and 1.0 arcsec, respectively. The Strehl values of the LGS at the mesosphere are indicated in column 3. The Py-WFS (extended) image of the LGS Strehl and FWHM values are indicated in columns 4 and 5. Compared to the bistatic case, the ALASCA monostatic architecture gives an intensity increase of the LGS image at the Py-WFS for the 1 kHz case which is 6-fold, while the shrinking of the LGS FWHM at the Py-WFS is a factor 4.4. Table 2.Performances of the LGS-AO loop, for the cases of 1 kHz and 2 kHz operation, with seeing of 0.7 and 1.0 arcsec
4.3Optical bench statusProcurement for the components is in progress; few items are experimenting some delays in the delivery, especially considering the well-known current problems with procurement of electronics components. In any case, no show-stopper so far have been identified. The optical bench is currently being integrated and tested at INAF laboratory in Rome. Figure 18 shows the current status of the optical bench. The mainstream optical path modules from DM to WFS are assembled, aligned and tested interferometrically. The LGS Pyramid WFS module is assembled and aligned, together with its WFS OCAM2S and Emergent Technologies scoring cameras. The SH-WFS module is being assembled. LGS double Axicon unit is under thermal performance tests. 4.4Next StepsOne important aspect that the project will address is the atmospheric scattering. The analysis of the effect of such event from free space laser propagation, considering both Rayleigh and Mie effects, has been outsourced to a specialized company with which the ALASCA team has a long heritage of collaboration. The activity is currently ongoing. In addition to that, the procurement of the components not yet ordered will be finalized shorty, especially considering the long lead time electronics components are experiencing due to the geopolitical situations. Subsystem testing of all the different modules not currently integrated on the optical bench will, then, be finalised before being integrated in the overall system at the INAF laboratory in Rome. The plan is to complete the system testing in Rome by the first quarter of 2023. 5OUTLOOK
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