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Presentazione Standard Di Powerpoint Copyright © Argotec S.r.l. 2020. All right Co reserved. - author and presenter: Cotugno presenter: Biagioand author Main author: author: SimoneMainSimonetti flight ofSLS towards the Moon Italian CubeSat technology to record the maiden ArgoMoon 1 Copyright © Argotec S.r.l. 2020. All right reserved. ARGOTEC Introduction 2 ARGOTEC Units and Locations Turin (IT) Headquarter – Engineering & R&D Labs Payloads SmallSat Avionics Cologne (DE) EAC – Training, Services and Operations Noordwijk (NL) ESTEC – Technical Support Training, Ops. R&D . 2020. All rightAll . 2020. 2020. All rightAll 2020. and Services S.r.l S.r.l Riverdale, MD (US) Argotec Argotec Argotec Inc – US brench © © 3 Copyright Copyright reserved.reserved. ARGOTEC Facilities Electronic Lab MultiLab Prototype Lab Thermal Lab Clean Room ISO 5 Mission Control Centre . 2020. All rightAll . 2020. S.r.l Argotec © COMPANY CONFIDENTIAL 4 Copyright reserved. Copyright © Argotec S.r.l. 2020. All right reserved. PLATFORM OVERVIEW 5 PLATFORM OVERVIEW Concept All-in-house . 2020. All rightAll . 2020. S.r.l Argotec © 6 Copyright reserved. PLATFORM OVERVIEW HAWK 6 - Deep Space Platform Deep Space communication Advanced maneuvering & attitude control and ranging capability High performance thruster with integrated RCS Compatible with DSN Exchangeable payload Tailored on mission needs 1.5 U of available volume Customized EPS and OBC with highly reliable space rated components . 2020. All rightAll . 2020. 2020. All rightAll 2020. S.r.l S.r.l Optimized for Deep space Radiation Argotec High protection structure Argotec © © 7 Copyright Copyright reserved.reserved. Copyright © Argotec S.r.l. 2020. All right reserved. HAWK 6 HAWK PLATFORM OVERVIEW - Deep Deep Space Platform 6U 8 Copyright © Argotec S.r.l. 2020. All right reserved. ARGOMOON OVERVIEW 9 ARGOMOON OVERVIEW Artemis-1 Mission - SLS ORBIT: 10,000 – 450,000 KM SLS ARTEMIS-1 MISSION LIFETIME: 6 MONTHS • PROVIDE AUTONOMOUS NAVIGATION AND POINTING BASED ON DETAILED PHOTOGRAPHY • VALIDATE NEW NANOSATELLITE TECHNOLOGIES IN DEEP SPACE • DEMONSTRATE HIGH HARDWARE RELIABILITY AND OPERABILITY . 2020. All rightrightAllAll . 2020. 2020. S.r.l S.r.l • PROVIDE HISTORICALLY SIGNIFICANT PHOTOGRAPHY OF Argotec Argotec © © ARTEMIS-1 MISSION • PROVIDE DETAILED IMAGERY OF ICPS, MOON AND EARTH MISSION OBJECTIVES MISSION 10 CopyrightCopyright reserved.reserved. ARGOMOON OVERVIEW Mission Overview ArgoMoon will be among the first to be deployed First Moon Flybys – 15000 km First phase – 10 hours – proximity maneuvers 5 Second phase – 6 months – On orbit testing 4 ICPS Trajectory - Heliocentric orbit M2 3 M1 PM 2 1 Deployment . 2020. All rightrightAllAll . 2020. 2020. S.r.l S.r.l Argotec Argotec © © PM: Proximity flight maneuvers Different CubeSat M1: Lunar Fly by Maneuver deployment point 11 Copyright reserved.reserved. Copyright M2: Final Maneuver for reentry trajectory ARGOMOON OVERVIEW Artemis-1 Mission - SLS Pointing Cameras towards ICPS Closure of the separation switches: power to the ICPS Targeted: system Tracking Mode Put in a Translunar Trajectory PS operational: Relative dynamic maneuvers 100m-500m proximity flight Geocentric orbit . 2020. All rightAll . 2020. Pictures of Earth and the Moon and . 2020. All rightAll 2020. S.r.l S.r.l validation of on-board technology Heliocentric disposal Argotec Argotec © © 12 Copyright Copyright reserved.reserved. Copyright © Argotec S.r.l. 2020. All right reserved. SUBSYSTEMS OVERVIEW 13 SUBSYSTEMS OVERVIEW Platform Overview MASS 14 KG VOLUME 6U - 911.5 MM 366 MM X 239 MM (WHEN DEPLOYED) GENERATED POWER 80 W THROUGH SOLAR PANEL STORAGE MEMORY 16 GB DOWNLINK BAND X-BAND DOWNLINK . 2020. All rightrightAllAll . 2020. 2020. S.r.l S.r.l DATA RATE 256 KPBS Argotec Argotec PROPULSION LMP103LT (PRIMARY PROPULSION) AND © © R134A (SECONDARY PROPULSION) 40° FIELD OF VIEW CAMERA, 2.5° FIELD 14 Copyright reserved.reserved. Copyright PAYLOADS OF VIEW CAMERA, RANGEFINDER SUBSYSTEMS OVERVIEW EPS and OBC&DH – In-House 30 KRAD RAD-HARD • 0.6 U - 0.8 KG • VOLTAGE 15V÷50V • OUT_PWR UP TO 80W (3.3V, 5V, 12V BUS) • LCL CIRCUITS FOR SEL MITIGATION • MPPT BASED ON COTS • 0.5U - 0.6 KG • DUAL-CORE SPARC V8 CPU . 2020. All rightrightAllAll . 2020. 2020. S.r.l S.r.l • 20 MBIT EEPROM EDAC • 16 GB NAND FLASH (+1000 PHOTOS) Argotec Argotec © © • INTEGRATED FPGA 15 CopyrightCopyright reserved.reserved. SUBSYSTEMS OVERVIEW Optical Payload – Imaging System 1.5 U – 1.2 KG + NARROW AND WIDE F.O.V. CAMERAS + 1 PX/CM RESOLUTION FROM 1 KM + INTEGRATED AUTOFOCUS ALGORITHM + DOUBLE CAMERA SYSTEM + BACKGROUND NOISE FILTER + FAST IDENTIFICATION OF THE TARGET + . 2020. All rightAll . 2020. 2020. All rightAll . 2020. ADCS POINTING OF THE SPACECRAFT S.r.l S.r.l + Argotec Argotec MULTIPLE TARGET IDENTIFICATION © © + FINE TRACKING FOR PHOTO SESSION 16 CopyrightCopyright reserved.reserved. SUBSYSTEMS OVERVIEW Autonomous Tracking and Pointing – In-House . 2020. All rightAll . 2020. S.r.l Argotec © 17 Copyright reserved. SUBSYSTEMS OVERVIEW REACT Argotec is developing an AI subsystems to handle off-nominal events or execute complex task without ground intervention for the ArgoMoon mission • An adaptive attitude control system for increased nanosatellite autonomy • Able to detect and react to reaction wheels failures • The system uses on Deep Reinforcement Learning to train . 2020. All rightAll . 2020. light and fast controllers based on S.r.l neural networks Argotec © 18 Copyright reserved. Copyright © Argotec S.r.l. 2020. All right reserved. CONCLUSION 19 CONCLUSION ArgoMoon on Artemis-1 Mission- SLS • Only European NanoSat on-board SLS • Collaboration with Italian Space Agency • Historic pictures of the first mission of SLS • High resolution pictures of Earth and Moon • Autonomous Navigation for tracking and pointing • Rad-hard in-house avionics technology . 2020. All rightAll . 2020. S.r.l • High data storage capacity Argotec © 20 Copyright reserved. Copyright © Argotec S.r.l. 2020. All right reserved. THANK YOU www.argotecgroup.com ! 21.
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