Current Status of Hayabusa2. Yuichi Tsuda, Project Manager, Hayabusa2 Project Japan Aerospace Exploration Agency
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1 Current Status of Hayabusa2 Yuichi Tsuda, Project Manager, Hayabusa2 Project Japan Aerospace Exploration Agency Small Body Assessment Group 18th Meeting, Jan.18, 2018
2 Present Status of Hayabusa2 (as of Jan.16, 2018) Traveled 2.79 billion km (w.r.t heliocentric inertial frame) Solar distance 1.25AU. Earth distance 2.08AU (RTLT=34min.) Just started the final Ion Engine burn before the asteroid rendezvous on Jan 10. Ion Engine Powered Cruise # 3 (Jan.10, 2018~Jun.5, 2018) Ryugu Orbit We are here! Hayabusa2 Trajectory Ion Engine Powered Cruise # 2 (Nov.22, 2016~Apr.26, 2017) Ryugu Arrival (Jun-Jul.2018) Sun Launch (Dec.2014) Earth Orbit Earth Swing-by (Dec.2015) Ion Engine Powered Cruise # 1 (Mar.22, 2016~May.20, 2016) 1
3 Recent / Near Future Cruise Operation <Recent Ops.> 2017 Apr.15 2nd IES Burn completed Apr IES trim burn May16-28 OpNav Jupiter/star Rendezvous calibration Phase May.30-Jun.1 start RCS (Jun.5, test burn 2018) Sep.5 Spacecraft clock reset Jul.18-Nov.14 Science instruments program update Nov.18,28 DSN-SSOC realtime Doppler transfer test Dec.2 DSN-UDSC uplink transfer test Dec IES test burn Ryugu Arrival 2018 (Jun.21-Jul.5, 2018) Jan.10 3rd term IES Burn Start <Near Future Ops.> ~May Ryugu first light Jun.5 IES burn completes. OpNav begins. Earth Sun IES Start IES Stop Sun Earth IES Start IES Stop IES Start IES Stop
4 Proximity Operation Plan Typical plan, Actual schedule fixed after arrival Approach Guidance Start(2500km) Ion Engine Stop Asteroid Arrival (20km) Gravity Measurement Descent (1km) Mid Altitude Observation Descent 1 (5km) MINERVA-II Deployment (50m) TD1 Rehearsal 1 (100m) Landing Site Selection1 TD1 (0m) TD1 Rehearsal 2 (50m) MASCOT Deployment (50m) Conjunction Period Mid Altitude Observation Descent 2 (5km) Pin-Point TD Campaign (max 4 descent) Crater Search Descent (1km) Kinetic Impact (500m) Pre-Impact Descent (1km) TD2 (0m) TD2 Rehearsal 2 (50m) Landing Site Selection2&3 MINERVA-II Deployment (50m) Hot Asteroid Period Asteroid Departure Spacecraft hovers at 20km altitude. All descent ops listed here are critical operations. 3
5 Prox Operation Training Campaign 2017 Landing Site Selection (LSS) Training (2Q-3Q, 2017) Purpose: Verification of LSS process Decision making framework/criteria, Tools and interface,... Trainee 100+ participants, JAXA engineering, Science (International), MASCOT team Training data Asteroid images (CG) based on actual observation operation plan Science data (Thermal, near infra-red, LIDAR data, gravity, ) Navigation data (position & velocity of S/C), Attitude data. Real-Time Integrated Operation (RIO) Training (4Q, Q, 2018) Purpose: Real-time operation training, Verification of ground support tools Touchdown operation, Impact operation, rover landing Trainee: all the operation staffs Training data Asteroid images (CG, real-time) Telemetry data (with communication delay) 4
6 Landing Site Selection Practice step1: God team creates Ryugoid Virtual asteroid Ryugoid in place of mysterious Ryugu. Assume from the formation history of Ryugoid. The shape and all the other properties were derived from the history. Each property was Intendedly deviated from known Ryugu property. The rotation state is randomly selected from public via Twitter. Shape model: 25cm resolution, 370 million polygon. Observation data generated based on actual operation plan & actual instruments performance. Generates attitude/trajectory simulation data based on operation plan Observation data and their ancillary data generated based on the simulation data. Goes through all the ground pipe line process as it really is. 5
7 Landing Site Selection Practice step2: Sci.&Eng. teams to solve the problem Observation (Simulated date generation) Modeling/Analysis Evaluation Landing Site Decision Jan-Jun, 2017 May-Aug, 2017 Jun-Aug, 2017 Sep 4, 2017 Touch Down Secondary Target Touch Down Primary Target 6
8 Surface feature of Ryugoid C.... Crater M.... Montes P.... Planitia R.... Rock Lumberjack C. Comb R. Apple R. Queen C. Sneezy C. Seven M. Ribbon R. Sleepy C. Axe R. Grumpy C. Dopey C. Forest Hemisphere hyb2_onc_180717_122656_tvf_l1a_lss_test Zone B Zone A Yodel M. Piece R. Snow White C. Doc C. Herb R. Hut Regio Happy C. Bashful C. Fairly Regio Mashroom R. Seven Dwarfs C.... Crater M.... Montes P.... Planitia R.... Rock Sneezy C. Queen C. Lumberjack C. Comb R. Apple R. Mirror P. Squire C. Yodel M. Horse C. Coal Hat R. Snowman C. Kingdom Hemisphere hyb2_onc_180717_083856_tvf_l1a_lss_test Zone D Zone D2 Zone C Seven M. White P. Bildung P. Boar R. Norm R. Burial Pit Grimms M. Coffin R. Prince C. 7
9 Landing Site Selection Practice step3: Landing Site Decision Two set of Mother spacecraft landing, MASCOT lander landing, MINERVA-II rovers landing sites are derived based on safety and scientific value. MI-1 E D2 D A B C MA-1 MA-2 MA-3 MA-4 Primary set:zone B, MA-2, MI-1 Backup set:zone D2, MA-1, MI-1 8
10 Real-time Integrated Operation Practice (RIO) TRIO (Training of RIO) Jan-Sep,2017: 18 run 13 crush 5 success/okey RIO Oct.2017-Apr.2018: total 30 run planned, 13 run 4 crush 9 success/okey. 9
11 RIO Example: MASCOT Release Operation Practice (Oct.19-20,2017) MASCOT Descent Aim Point View of Optical Navigation Camera ONC-W1 Descent start (-1m/s) Slow Down (-0.1m/s) 60m arrival/release Ascent to 3km Hovering 10
12 Imagining Ryugu Space Art Contest Can you predict Ryugu appearance better than scientists? 11
13 Thank you! 12
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