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The Pan-STARRS Moving Object Processing System (& Science) Robert Jedicke (for the Pan-STARRS collaboration) Institute for Astronomy University of Hawaii 2004 September 29 IMPACT IMPACT IMPACT The Pan-STARRS Moving Object Processing System (& Science) Robert Jedicke (for the Pan-STARRS collaboration) Institute for Astronomy University of Hawaii 2004 September 16 The Pan-STARRS Moving Object Processing System (& Science) (& Science) Robert Jedicke (for the Pan-STARRS collaboration) Institute for Astronomy University of Hawaii 2004 September 16 Bigger Further Slower Dumber Bigger Further Slower Dumber DEFINITIONS icier COMETS ASTEROIDS dirtier DEFINITIONS Near Earth Objects (NEO) NEO ZONE Perihelion < 1.3AU (about 130 million miles) DEFINITIONS Potentially Hazardous Objects (PHO) PHO ZONE MOID < 0.05 AU (about 5 million miles) PHO Orbit Earth Collision at perihelion Non-Collision ‘PHO’ Orbit Not at Earth’s orbit at perihelion 1995 CR DEFINITIONS Death Plunge Objects (DPO)* * Not an official acronym Solar System Animation #3 DEFINITIONS Trojans Main Belt Objects Trojans DEFINITIONS Centaurs Trans-Neptunian Objects (TNO) Comets Short Period Comets Halley Family Comets Long Period Comets DEFINITIONS Oort Cloud The Pan-STARRS Moving Object Processing System (MOPS) Selected PanSTARRS’s Top Level Science Requirements • MOPS shall create and maintain a data collection of detections and object parameters (e.g. orbit elements, absolute magnitudes) for >90\% of the PHOs that reach R=24 for 12 contiguous days during the course of PanSTARRS operations. • MOPS shall create and maintain a data collection (DC) of detections and object parameters (e.g. orbit elements, absolute magnitudes) for >90% of the members that reach R=24 12 contiguous days within each class of solar system object (Main Belt, Trojan, Centaur, TNO, Comet, etc, except NEO and PHO) during the course of Pan-STARRS operations. Selected PanSTARRS’s Top Level Science Requirements • MOPS shall create and maintain a data collection of detections and object parameters (e.g. orbit elements, absolute magnitudes) for >90\% of the PHOs that reach R=24 for 12 contiguous days during the course of PanSTARRS operations. • MOPS shall create and maintain a data collection (DC) of detections and object parameters (e.g. orbit elements, absolute magnitudes) for >90% of the members that reach R=24 12 contiguous days within each class of solar system object (Main Belt, Trojan, Centaur, TNO, Comet, etc, except NEO and PHO) during the course of Pan-STARRS operations. Why? REASON #1 REASON #2 SPACEGUARD GOAL SPACEGUARD GOAL NASA NEO SDT Pan-STARRS & PHOs • 99% completion of PHOs with D>1km 90% reduction in residual global impact risk • 90% completion of PHOs with D>300m 50% reduction in sub-global impact risk REASON #3 REASON #4 Existing Surveys Existing Surveys – Step 1: Discovery & Identification LINEAR White Sands, NM) LONEOS Flagstaff, AZ NEAT/JPL Haleakala, Maui CSS -South Australia NEAT/JPL Palomar, CA CSS - North Mt. Lemmon, AZ Spacewatch Kitt Peak, AZ UHAS Mauna Kea, HI • 3-5 images/night • Linear motion • Very low falsepositive rate Existing Surveys – Step 2 Linkage & Orbit Determination MPC • Links detections to known objects • Identifies new objects • Fits orbits to all objects with new detections • Much more… Existing Surveys – Step 3 Impact Risk Assessment • Refine orbits • Calculate impact probability Moving Object Processing System Pan-STARRS Telescopes & Survey Image Processing Pipeline MOPS Impact Probability • Fully integrated • Detection, attribution, linking, orbit identification • Orbit fitting • Parallel synthetic data analysis Real-time efficiency/bias Moving Object Processing System Moving Object Processing System Moving Object Processing System • MPC requires that reported detections be real forces Pan-STARRS to obtain 3 images/night reducing total sky coverage reducing total discoveries • Difficult to control/monitor system efficiency introduce synthetic objects into data stream determine efficiency in real time monitor system performance in real time PanSTARRS Asteroid Surveying 7 • 10 asteroids within range of PanSTARRS 2 • ~200 / deg @ V=24 @ on ecliptic 7 • 10 detections / month (20X current rates) Cumulative Observations 160,000,000 140,000,000 120,000,000 100,000,000 80,000,000 60,000,000 PS1 Starts 40,000,000 20,000,000 2006 2005 2004 2003 2002 2001 2000 1999 1998 1997 1997 1996 1995 0 Observing Cadence • Every survey mode obtains at least two images at each location separated by a Transient Time Interval (15-30 minutes) serendipitous positions & colours • Solar system survey re-visits each location after 3-6 days obtain 3-4 nights/month ~12 day arc Moving Object Processing System • 2 detections/night with multi-night linking increased sky coverage push deeper into noise more objects •synthetic data real-time system monitoring efficiency determination correction for selection effects Transient Detection (IPP) 4 Telescopes Stationary + Combined + Static Transients Moving + Transient Types Supernovae/GRB Difference Slow Asteroidal Object Normal Asteroidal Object Cometary Object Death Plunge Object Fast Asteroidal Object Linking Detections Day 1 1 Field-of-view 1500 real detections + 1500 false detections Linking Detections Day 5 1 Field-of-view 1500 real detections + 1500 false detections Linking Detections Day 9 1 Field-of-view 1500 real detections + 1500 false detections Linking Detections •Brute force (MPC) approach 100X Pan-STARRS computing power • kd-tree (CMU) approach ~1/3 Pan-STARRS computer power Orbit Determination • Must include – All major solar system perturbing bodies – Full error analysis • Two available solutions – AstDys (Italy) – JPL (USA) Data Storage • Large by most astronomical standards • Small in comparison to Pan-STARRS (~1%) 500 TerraBytes Synthetic Data • Inject synthetic objects into MOPS parallel to real data analysis monitor system efficiency for correcting observational selection effects monitor system performance to flag unusual behavior Synthetic Data • Synthetic model matches real distributions all asteroid and comet types realistic orbit and size distribution realistic shape, rotation periods, pole orientations + ‘unusual’ orbits e.g. hyperbolic interstellar, retrograde main belt, distant Earths MOPS: Known Object Attribution MOPS: Synthetic Detection & Noise Generation MOPS: Orbit Determination & Attribution Loop MOPS: Linking New Detections The Pan-STARRS Solar System Survey & Science Solar System Survey Locations 19:00 HST 00:00 HST 05:00 HST Evening Sweet Spot Opposition Morning Sweet Spot Pan-STARRS & NEOs/PHOs • Tens of thousands of NEOs Size-frequency distribution Orbit distribution Source fitting Genetic families? Pan-STARRS & the Main Belt • Pan-STARRS will find as many objects in one lunation as have been identified since the discovery of Ceres in 1801 Pan-STARRS & the Main Belt • 10,000,000 MB objects in ten years Size-frequency distribution Orbit distribution New small asteroid families Asteroid/comet transition objects Asteroid collisions Pole Orientations Rotation Rates Shapes Pan-STARRS & Trojan Asteroids 6 1,000,000 5 100,000 4 10,000 Series1 Known Series2 Pan-STARRS 3 1,000 2 100 1 10 01 1 Jupiter 2 Saturn 3 4 Uranus Neptune Trojans of all giant planets L4 & L5 swarm statistics Genetic families SFD through rollover at H~11 Jewitt 2003, ‘Project Pan-STARRS and the Outer Solar System,’ EMP Pan-STARRS & Comets • Pan-STARRS will find ~10X as many comets per year as all existing surveys • 1,000’s of comets in ten years operation Dormant detections at large distance Size-frequency distribution Orbit distribution • INTERSTELLAR ! ! ! Pan-STARRS & Comets • Comet designation problem • New Proposal Comet Jedicke-XXX X=(0-9,a-z,A-Z) (base 62) allows for ~240,000 comets P/Jedicke 1996A1 Pan-STARRS & TNOs • ~20,000 TNOs Inclination distribution Size-frequency distribution Orbit distribution / dynamical structure More Plutos? ~100 wide binaries Pan-STARRS & Distant Planets New Plutos 320AU New Earths 620AU (50AU) New Neptunes 1230AU (130AU) New Jupiters 2140AU (340AU) Jewitt 2003, ‘Project Pan-STARRS and the Outer Solar System,’ EMP Pan-STARRS Minor Planet Summary 8 10,000,000 7 1,000,000 6 5 100,000 Series1 Known 4 10,000 Series2 PS 1 Year Series3 PS 10 Years 3 1,000 2 100 1 10 01 1 2 3 4 5 6 7 8 9 10 PS1 - 2006 PS4 - 2008 Coming soon to an island near you. Pan-STARRS Problem: Pan-STARRS plans on using a very wide ‘Solar System’ G filter but is required to reach R=24. Assuming that the R-filter transmission is 100% in the range [R1,R2] and 0% outside that range and that the G-filter has similar performance in the range [G1,G2] where G1<R1 and G2>R2, what is the ratio of the required exposure times in the two filters to reach R=24 in the AB magnitude system? Assuming that Vega is a black-body, what is the answer in the Johnson system? Make other reasonable assumptions as necessary