ROBOTICS AND LUNAR EXPLORATION Ayanna M. Howard, Ph.D. Human-Automation Systems Lab School of Electrical and Computer Engineering Georgia Institute of Technology Acknowledgements: Dr.
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ROBOTICS AND LUNAR EXPLORATION Ayanna M. Howard, Ph.D. Human-Automation Systems Lab School of Electrical and Computer Engineering Georgia Institute of Technology Acknowledgements: Dr. Edward Tunstel, Lead Engineer, MER Mobility Team Dr. Paul Schenker, Manager, Robotics Space Exploration Technology Program Why Robots? • WHY NOT JUST HUMANS FOR PRE-CURSOR LUNAR MISSIONS?? • Has been PROVEN that Human Control is NOT Safe!! • When steering commands are delayed by communications there is a tendency for the operator to over-steer and lose control. • It was shown that with a communication delay corresponding to round trip to the Moon (about 2 1/2 seconds) the vehicle could not be reliably controlled if traveling faster than about 0.2 mph (0.3 kph) [Adams 1961] Why Robots? • WHY ROBOTS FOR SORTIE MISSIONS?? • A complex extended mission will require more tasks than humans can support without help. • Crewmember time will be a very valuable resource, so mundane tasks should be minimized. This will allow the crew to apply their expertise where it is most needed. • Extra-vehicular activity is particularly risky for humans, but will be unavoidable for a complex mission. – Spacesuits restrict mobility, dexterity, and visual field – Suit pressurization opposes bending motions, reducing effective stamina – Limited time during EVA, plus time for pre-breathing Rover Functionality • • More increasingly, robotic vehicle autonomy is necessary for ensuring science return and achieving overall success of planetary surface missions Recent and planned missions include requirements that rely on autonomous mobility and manipulation technologies to achieve mission success – Mars Pathfinder (MPF) (Sojourner rover): • traverse to science targets to acquire spectroscopic measurements – Mars Exploration Rover (MER): • traverse to new locations over terrain of some reference complexity and accurately place instruments onto science targets • maintain estimated position knowledge within some % of distance traversed – Mars Science Laboratory (MSL); ExoMars MER Benchmark for Rover Autonomy • MER represents the longest deployment of planetary rovers in remote planetary surface environments. • A new benchmark in planetary robot autonomy and human-robot systems (in addition to a landmark in planetary in situ scientific exploration) • Assess rovers’ performance (surface navigation and instrument placement) to facilitate understanding of future robotic systems by providing metrics derived from Mars performance data for Spirit and Opportunity. Surface Operations • Rover technologies can be classified based on four common technologies Surface Mobility (Mobile Autonomy) Terrain assessment, path planning, visual servoing (Mobility Mechanization) Science Perception, Planning & Execution On-board and ground tools; data analysis, target selection, operations planning and execution Extreme terrain access, energy efficiency Human-Robot EVA Interactions Tele-operation and human supervision of robotic explorers Robotic work crews Instrument Placement and Sample Manipulation Position sensors, collect and process samples May include sample containerization and return-rendezvous phases Surface Mobility Movement is a key requirement for autonomous planetary rovers. Focus is to enable planetary rovers to traverse long distances on challenging terrains safely and autonomously. • Trade-offs on design include: QuickTime™ and a Motion JPEG OpenDML decompressor are needed to see this picture. HumAnS Lab, GeorgiaTech • – – – – – – Maneuverability Traction Climbing ability Stability Efficiency Environmental impact Characteristics include: – – – – – – Distance/range Speed Terrain accessibility (slopes, obstacles, texture, soil) Load carrying capability Agility (turn radius) Access (vertical, sub-surface, small spaces, etc.) Science Perception, Planning, Execution • Provide ground tools for scientists to plan days events, while allowing generation and robust execution of plans with contingencies, concurrent activities, and flexible times • Characteristics Include: • Sensing • Analysis (e.g. chemical analysis) • Data processing • Understanding of Context, Knowledge, and Experience Se ns or, te rrain-inte raction, and navigational control m ode ls drive e arly ope rational s cenario ass e s s m e nt and de sign validation Modeling Global Site Knowledge Hypothesis Generation In-Situ Measurement Hypothesis Testing Human-Robot EVA Interactions • Characteristics – Ground based supervised autonomy (versus tele-operation) • – – – Operator may enter planning, monitoring, and control at multiple levels Proximate telepresence Shoulder-to-shoulder interaction Robot assistants QuickTime™ and a Animation decompressor are needed to see this picture. HumAnS Lab, GeorgiaTech Instrument Placement/Sample Manipulation Arm placement and object manipulation involves touching a specific point in 3D space, grasping an arbitrarily oriented object in 3D space, and moving an object from one location to another. The CHALLENGE Get there efficiently and safely And, move the arm so that it does not try to violate its own joint limits And ensure that it does not hit itself or the rest of the robot, or any other obstacles in the environment • Common Characteristics Include: – Mass and volume – Fragility, contamination, reactivity – Manipulation technique: Torque, Precision, Complexity of motion – Repetitive vs. unique – Time – Moving with minimal disturbance 1.6 m ~2.1 m Capability Benchmarks: MER to MSL 1.2 m Mars Exploration Rover 1.7 m Mars Science Laboratory Landed Mass 174 kg ~600 kg Autonomous Traverse Rates 17.5-34.5 m/hr 89-100 m/hr Designed Driving Distance ~4500 m 5000-10,000 m Approachability 2.93 m/sol 6.67 m/sol Power/Sol 400 - 950 w/hr ~2400 w/hr Instruments (#/mass) 7/5.44 kg 6-9/65 kg Data Return 50-150 Mb/sol 500-1000 Mb/sol Current State-of-the-Art • Autonomous mobility and sample access – MER mobility: 10-120 m/sol to commanded point with > 90% success, < 20 degree slopes, sparse obstacle field – MER visual odometry: ~2% accuracy over distance traveled – MER sample access: RAT, wheel scuffing of soil – Deep Space 2: Small, sub-surface micro probe, ~50cm access • Autonomous instrument deployment – MPL arm: ~2 m reach, 4 DOF, operated from fixed platform – MER arm: 90 cm reach, 4 DOF, operated from mobile base • On-board autonomous science – Human-commanded on per-sol basis – Fixed sequences • Human-robotic field science – No operational experience • Human-robot interaction – Sojourner/MER: Ground teleoperation – MER: Commanded on per-sol basis => Laboratory, and some field, demonstrations of long-range navigation (< km per command cycle), 7DOF arms, meter-deep drilling, single instrument placement, autonomous science planning and execution, robotic assistants, etc. Challenges to Mobile Autonomy autonomous traverse route goal AUTONOMOUS TRAVERSE: Autonomous traverse, obstacle avoidance, and position estimation relative to the starting position. Single vehicle to access all terrain types, cover long distances, and carry/deploy a payload. partial panorama goal cameras & spectrometer processing and caching drilling & scooping APPROACH & INSTRUMENT PLACEMENT: Autonomous placement of a science instrument on a designated target, specified in imagery taken from a stand-off distance. Precise contact measurements and autonomous sample manipulation. Drilling to 1000m depth. Visual servoing/approach to multiple targets in single command cycle. ONBOARD SCIENCE: Autonomous processing of science data onboard the rover system, for intelligent data compression, prioritization, anomaly recognition. Human level cognition and perception of science opportunities. SAMPLING: Sampling, sample processing, and sample caching through development of controls for new system components. Challenges: Lunar Characteristics • Gravitational Characteristics • Low gravity: 1/6 Earth’s - low energy locomotion • Rotational/Orbital Characteristics • Communications easy from near side, difficult from far side, periodic at poles • Long days, long nights: 14.6 days light, 14.6 days dark • Sun skims horizon at poles • Permanent shadows in polar craters • Earth-to-Moon Characteristics • 2.5 second round-trip speed-of-light delay Challenges: Lunar Characteristics • Impact Craters • Microcraters: 10-8 - 10-3 meters • Regolith craters: 10-2 - 103 meters • Large craters/Impact basins - 102 - 106 meters • Volcanic Channels, Collapsed Lava Tubes, Mountains • Regolith • 2-8 meters deep in maria regions • 15 meters deep in lunar highlands • Dust • Extremely fine, electrostatically charged Capability Trends Time Estimates for Space Robotics Metric Technology / Sub-Capability SOA Target Value Available Distance traveled per day Autonomous Navigation Aerial Traverse 100m 1km 1km 10km 2009 2015 Difficulty of terrain that is accessible Autonomous Navigation VL1 >VL2, cliffs, craters 2015 Drilling depth Sub-Surface Access 10Õs cms 10-20 ms 2013 Autonomously controlled manipulator degrees of freedom Instrument Placement, Human-Robot Interaction 7 10Õs 2020 Command cycles per sample acquired Instrument Placement, Field Science 3-6 1 2009 Command cycles per sample processed Field Science Dozen s 1-2 2013 Command cycles to survey/characterize site Field Science >100 <20 2020 Percent of interactions interpreted correctly by robot Multi-modal communication Behavior tracking 80% 70% 95% 95% 2020 # robots supervised per human Human-Robot Field Science Co-located Interaction <<1 3-5 2020 QuickTime™ and a YUV420 codec decompressor are needed to see this picture. EXAMPLE: Rover Metrics LEMUR, JPL Tethered crater descent L im b e d e x c u r s io n r obot f or Extensib le cooperative multi-rob ot work system Robot Work Crew s u r fa c e Q u ic k T im e ™ a n d a decom p r essor a r e n e e d e d t o s e e t h is p ic t u r e . Traversesability (relative to rock area density) a n d sp a c e Cliffhanger — s t ru c t u r e s chang e a b le has Q u ic k T im e ™ a n d a decom p r essor a r e n e e d e d t o s e e t h is p ic t u r e . Dante II Q u ic k T im e ™ a n d a deco m pr essor ar e n e e d e d t o s e e t h is p ic t u r e . endef f ect o r s e n s in g / t o o lin g Q u ic k T im e ™ a n d a decom p r essor a r e n e e d e d t o s e e t h is p ic t u r e . Cliff-bot Q u ic k T im e ™ a n d a decom p r essor a r e n e e d e d t o s e e t h is p ic t u r e . Q u ic k T im e ™ a n d a decom p r essor a r e n e e d e d t o s e e t h is p ic t u r e . 70+ degree navigable cliff descent / ascent Q u ic k T im e ™ a n d a decom p r essor a r e n e e d e d t o s e e t h is p ic t u r e . Q u ic k T im e ™ a n d a decom p r essor a r e n e e d e d t o s e e t h is p ic t u r e . Au t o n om o us u rb a n Q u ic k T im e ™ a n d a decom p r essor a r e n e e d e d t o s e e t h is p ic t u r e . L EM UR 1 15 kg, 1.5 meter wheel, 50 cm/sec r econr eb ot 50% slope Q u ic k T im e ™ a n d a decom p r essor a r e n e e d e d t o s e e t h is p ic t u r e . 40- Inflatable Rover 5 0 d e g r e e s lo p e acces ( in LSR Nanorover s im u la t e d Q u ic k T im e ™ a n d a decom p r essor a r e n e e d e d t o s e e t h is p ic t u r e . Q u ic k T im e ™ a n d a decom p r essor a r e n e e d e d t o s e e t h is p ic t u r e . Q u ic k T im e ™ a n d a decom p r essor a r e n e e d e d t o s e e t h is p ic t u r e . Re c o n f ig u r a b le r o v e r , URBI E s a m p le c a c h e tr a n s f e r ) 7 Kg, 1 meter footprint, composite construction, lightweight rover Sa m p l e Re t u r n VL2 Self-righting 2 kg rover Ro v e r 1 - 3 commands / ops cycle MSL 3 - 10 commands / ops cycle 10 + commands per operational cycle M ER Sojourner Hyperion VL1 1 Background image: MER 2 with Sojourner model 10 100 Mobile Robot Range (meters) 1000 NOMAD 10000 Sortie Missions: Robotics Proximate Telepresence • In many missions, the humans will be near the robots but will be supervising them from a safe distance (e.g., in a habitat or on orbit). To facilitate the interaction, the robots should have capabilities similar to humans (especially in terms of manipulation) and the level of control between robots and humans should be highly flexible (“sliding autonomy”). Situational awareness of the supervisor needs to be high, which can be facilitated with both multi-modal feedback and high-level interpretation (by the robot) of sensor data. Safeguarding to prevent harm to the robots is critical. Shoulder-to-Shoulder Interaction • In some missions, humans and robots will be co-located on site, working together. At a basic level, the robots will need to understand and communicate with the astronauts using both speech and gesture. In addition, in many cases they will need to infer (without communication) the behaviors and intentions of the astronauts and alter their activities accordingly to support the astronauts’ goals. Safeguarding to prevent harm to the humans is critical. (Some risk) Surface EVA Assistance • NASA-JSC Boudreaux – an Extra-Vehicular Activity (EVA) Robotic Assistant • Specific sub-capabilities include: – Site development (survey, excavation, resource deployments) – Site maintenance (inspection, repair, assembly, materials transport) – In situ resource production (robotic support to extraction, transport, manufacturing) – Field logistics and operations support (materials & equipment transport & warehousing) – Human-robot interaction (H/R task allocation, teleoperation, remote supervisory control, etc.) QuickTime™ and a YUV420 codec decompressor are needed to see this picture. JSC Why EVA robots must assist humans • Humans are necessary for surface EVAs – Adaptability, Intelligence, Dexterity • Robots are necessary for surface EVAs – Pack mule, extra hand, situational awareness – Put robots at risk instead of humans QuickTime™ and a YUV420 codec decompressor are needed to see this picture. JSC Robot Capabilities • Have a robot assist an astronaut in deploying science instruments (e.g. geophones) • Various forms of interaction: voice commanding, gesture recognition, dialogue, full autonomous mode, traded autonomy • Various forms of Capabilities: mobility, manipulation, autonomous traversal of rugged terrain, tracking of suited crew member QuickTime™ and a MS-MPEG4v2 Codec decompressor are needed to see this picture. Robonaut, JSC Benefits for Sortie Missions • Robotic ISRU, robotic precursor preparation and ongoing robotic mission support are enabling for due to impact on sustainability and affordability. • Human safety is enhanced through precursor robotic site preparation. • Field operations productivity is enhanced through robotic “mule” support and robotic mobile communication networking. • Astronaut productivity is enhanced by lowering maintenance and inspection overhead assigned to human crew. • Ground-crew interaction productivity is enhanced by improved human-robot interfaces. Summary State-of-the-Art • Robotics has not been used for lunar exploration. • State-of-art can be indirectly measured from sub-capabilities with terrestrial deployment, TRL6 and below: – Site development: Autonomous robotic excavation and site shaping has been demonstrate by joint CMU – Caterpillar front loader system. – Site development: Communication infrastructure deployment by various university research groups in the DARPA Centibots program has set up networks using robot teams in unexplored urban areas. – Site maintenance: Dexterous manipulation under teleoperation has been demonstrated in analog environments by both Ranger and Robonaut research teams with astronaut glove-level dexterity and 6x slowdown. – Field logistics and operations support: Long-distance autonomous navigation has been demonstrated on the order of 100km total distance traveled. – Field logistics and operations support: Architectures for perception, planning and control have demonstrated efficacy in Mars-analog tests at JPL and Ames. Deliverables for Capability Metrics for Sortie Missions Metric Technology / Sub-Capability SOA Target Value Available # human interventions per task Site development & maintenance > 10 <3 2012 Average distance Field logistics and navigated per operations human intervention support <100m 1000m+ 2020 Proportion of navigation goals achieved Field logistics and operations support 96% (MER) 99% 2020 % reduction of human cognitive load Human-robot interaction << 10% 25% 2008 Maximum parallel human-robot supervisions Human-robot interaction ~1 3+ 2020 Cubic meters excavation per hour Robotics for ISRU ? ? 2015 Conclusions NASA manned and unmanned missions will be carrying out increasingly challenging tasks on the lunar surface: • • • • • Habitat construction and long term habitation Mining and in-situ resource utilization Deep drilling Scientific laboratory tests currently done only on earth Biological and habitability analysis Robotics is key for providing both enabling and enhancing capabilities necessary for achieving the goals of these future missions.