DustCube. AIM Industry Days. (22-23 February 2016) Franco Pérez Lissi DustCube Team - University of Vigo
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1 DustCube AIM Industry Days (22-23 February 2016) Franco Pérez Lissi DustCube Team - University of Vigo franco.perez@humsat.org
2 DustCube TEAM
3 DustCube Project Consortium University of Bologna Orbit Dynamics Attitude Control Systems Navigation Control Systems Project Management System Engineering SC Platform SC Operations Optical Payload Design Scientific analysis Environmental Testing
4 DustCube Project Consortium (1 / 4) UVIGO CubeSats Experience in 8 years: 3 CubeSats launched and operated until 2016 SERPENS: 3U (Fully OperativeNOW) Launched with JAXA, through the ISS 19/08/2015 Xatcobeo: 1U (Operated for 2.5 years, Re-Entered on 01/09/2014) Launched with ESA Vega HUMSAT-D: 1U (Operated for 1.2 years, OPS Finalized on 02/2015) Launched with Dnepr 11/2013 On-going developments: HumSat2.0 Payload: FemtoXat ⅓ U (Modular Cubesat) Second Generation SDR payload (Expected Launch in 2017) for HUMSAT. (End of 2016) SatNet: Open Source Ground station network (Final testing. Operative on 03/2016) ESA ESEO Satellite - Ground Station Node Pontevedra Smart City Sensors Network deployment. Development of Highly adaptable EGSE tools for SC Testing Developments of CubeSats Telemetry analysis tools
5 DustCube Project Consortium (2 / 4) ALMASat (ALma MAter Satellite) Demonstrator, successfully launched on February 13th, 2012 ESEO satellite GPS Receiver and OD, as part of the payload package (in collaboration with SITAEL) Ground Stations design. Target research areas: Micropropulsion systems Cold-gas, flown on ALMASat-1 in 2012 Monopropellant warm-gas, under development GPS Receivers and Autonomous Navigation Systems Ground Segment/Station Technologies and Mission Control Centers AODCS simulation tools University of Bologna
6 DustCube Project Consortium (3 / 4) RadioScience Experiments Orbit Determination Planetary Exploration University of Bologna
7
8 DustCube SCIENCE
9 SCIENCE Objectives Mission Phase Objectives INH + INH-CTS + RNH Natural dust environment characterization Particles size, shape and distribution Particles Speed Surface Topology Pre-Impact Didymos system images Impact Particles size, shape and distribution characterization High-Res Impact Images Impact Ejecta monitoring (dn/dv concentration) INH + RNH Post Impact Plume evolution monitoring Laser Altimetry Post-Impact surface Images INH + RNH + TOF Pre-Impact Supporting Instruments
10 Payload (Remote Nephelometer + InSitu Nephelometer) Telescope FOV Laser Beam Samples Inlet Payload Design (In-Situ Nephelometer (INH) + Remote Nephelometer (RNH) ) INH : Instrument Inherited from PI-Neph (DEVOTE, NASA Mission) Instrument miniaturization for a 1/2U CubeSat volume equivalent RNH: Instrument enhancement for remote sensing Scattering data from remote particles Technology validation of an altimetry laser system use for both surface recognition and navigation.
11 DustCube CONOPS
12 Concept of operations Set of alternatives for INJECTION Phase, based on injection complexity (Backed-up with numerical models) Set of alternatives for IMPACT Phase, based on probability to be impacted by ejected plume, and navigation complexity (Backed-up with Orbital and Environmental analysis )
13
14 DustCube SpaceCraft
15 S/C Configuration 1 x 3U CubeSat Payload RNH Heritage Platform + NAV Payload INH PROP ADCS Samples Inlet Optical Navigation Cold Gas Propulsion 3-axis pointing Reaction wheels Start-trackers Sun-sensors Payloads Two deployable solar panels Estimated power generation of 15W
16 Proposed inherited Platform for DustCube System Reliability: > 4 Years in Orbit, more than EXECUTED COMMANDS Inhouse subsystems development + COTS Critical components = RAD-HARD Inhouse OBSW: On Board SW FDIR implementation (Failure detection, isolation and recovery) High level of autonomy High modularity for new payloads 40 different Telemetries 84 Telecommands direct and scheduler programming Exhaustive system engineering effort and AIT: TLYF (Test Like you Fly) E2E EMC Testing ECCS Tailored Methodology for CubeSats developments LOW COST! (Lowering the cost, without compromising reliability) GSSW (Ground Segment Software) based on PUS (Packet Utilization Standard) Inhouse developments COMMs Protocol Station Manager Telemetry - TM Viewer Telecommand Manager Telecommand translator for programming
17 Fresh data from SERPENS Cubesat (Proposed Platform) Snap shot of SERPENS TM Viewer during S/C pass over Vigo (Thursday 18/02/2016) Executed Commands on scheduler (since 09/2015) Downloaded Data in the communication pass: Environmental data collected from HUMSAT sensors deployed in ANTARCTICA + Chile + California + Spain. Payload measurements of Global VHF radio interference on the Amateur band to globally map the jamming sources.
18 Fresh data from SERPENS (Antarctica data and sensors) Figure. Humsat sensor Figures. Data gathered from Antarctica sensors Figure. Antarctica spanish base sensor location
19 University of Bologna DustCube Project Thank you for your attention! Franco Pérez Lissi DustCube Team - University of Vigo franco.perez@humsat.org
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