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Human Robotic Systems (HRS): Robotic ISRU Acquisition Element
<p>During 2014, the <em>Robotic ISRU Resource Acquisition </em>project element will develop two technologies:</p><ul><li>Exploration Ground Data Systems (xGDS)</li><li>Sample Acquisition on Asteroids, Mars, Moons of Mars, and Lunar Cold Traps</li></ul><p>A primary technology of this element is development of HRS&rsquo;s Exploration Ground Data Systems (xGDS) software, a set of planning, monitoring, archiving, and search tools for dealing with data sent to or received from robotic spacecraft or crew systems.&nbsp; xGDS is being matured through technology development under HRS (with STMD funds) and field-tested with funds from the Human Exploration and Operations Mission Directorate (HEOMD) and Science Mission Directorate (SMD).&nbsp; The outcome of this development will be that the desired parts of the xGDS system (likely the traverse planner, real time plotting, and raster mapping tools) will be ready to be infused into the lunar Resource Prospector Mission (RPM).&nbsp; The scope of FY14 xGDS work includes maturing time delayed image and video processing and archiving tools and adding support for mobile devices.&nbsp; During 2014, xGDS will support the AES-funded Regolith and Environment Science and Oxygen and Lunar Volatile Extraction (RESOLVE) payload thermal vacuum chamber testing the SMD-funded Mojave Volatiles Prospector (MVP) project.&nbsp;</p><p>Another technology under this element will develop regolith sampling and excavation for reduced and low gravity environments.&nbsp; The objective for this work in FY14 is to acquire representative samples of target bodies in order to characterize the regolith for ISRU prospecting purposes which would also benefit science objectives and other relevant Strategic Knowledge Gaps (SKG&rsquo;s). The requirements of the Advanced Exploration Systems (AES) lunar Resource Prospector (RP) are focused on a lunar South pole mission near the impact site of the recent Lunar CRater Observation and Sensing Satellite (LCROSS) mission in order to obtain ground truth on the lunar surface.&nbsp; Orbital data from neutron spectrometers shows that most of the detected hydrogen on the moon is in these crater floor cold traps. The goal is to confirm the existence of volatiles such as water, hydrogen and helium in the regolith at the lunar poles.&nbsp; Other target bodies such as asteroids and Mars&rsquo; moons will also need prospecting and characterization. One of the primary potential uses of the returned asteroid in the Asteroid Initiative is for ISRU demonstrations in lunar orbit.&nbsp; Sampling devices will be needed to prospect the asteroid for useful resources, such as water on a carbonaceous condrite. The Mars&rsquo; moons and Mars itself are also of interest for ISRU purposes and can be sampled with robotic devices or by human crews to determine the ISRU value of their regolith.</p><p>Regolith excavation and sample acquisition in low gravity environments ( micro-G, 1/3 G, 1/6th G) is difficult due to the lack of reaction force from the weight of the excavation robot.&nbsp; On Earth, excavators are typically large and heavy to take advantage of this large reaction force to counter-act the digging forces. In space, new methods of digging and sampling must be found, due to their light weight in low gravity environments.&nbsp; Percussive excavation is one method for reducing digging forces, and in FY14, the HRS project will test interfaces for a large percussive excavation end effector: the Vibratory Implement for Percussive Excavation of Regolith (VIPER) which is designed to be mounted on the All-Terrain Hex-Limbed Extra-Terrestrial Explorer (ATHLETE) robot from JPL. The VIPER was designed and fabricated by HRS. A smaller percussive excavation implement called Badger, will be operated on the Centaur 2 mobility robot with a positioning mechanism. Firs
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Human Robotic Systems (HRS): Robonaut 2 Technologies Element
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The goal of the Robonaut 2 (R2) Technology Project Element within Human Robotic Systems (HRS) is to developed advanced technologies for infusion into the Robonaut 2 project leading to new capabilities for Robonaut. In FY14, HRS and the Technology Demonstration Mission (TDM) Human Exploration Telerobotics (HET) will collaborate to deliver a mobile IVA Robonaut 2 to ISS.

During 2014, the “Robonaut 2 Technologies” project element will develop two technologies:

  • Mobile IVA Robonaut 2
  • Natural User Interfaces for Advanced Telerobotic Operations

The primary work area in this project element is to contribute to sending a mobile IVA Robonaut to the International Space Station (ISS) and to begin using it as a mobile system.  The main area where HRS will contribute to Robonaut 2 in FY14 will be in the area of battery development.  HRS will perform component testing of the engineering development unit (EDU) and complete assembly of the certification unit battery. The development will eventually lead to a robotic system moving and working safely in the same space as Astronauts on ISS. 

The second work area under this project element will be to use body-tracking input devices (i.e. Microsoft Xbox Kinect and accelerometer gloves) to immerse an operator in an accurate virtual model of the robot’s environment, capture the intent of the operator, and safely execute mobility and manipulation tasks suitable for platforms such as Robonaut 2. Initially, the operator’s head position will be tracked in order to render an appropriate point of view in the virtual environment. Next, model-based recognizers will be developed and trained to detect gestures by the human operator and trigger autonomous behaviors on the robotic system. Initial efforts will use the Kinect sensor, with additional potential investigations into other similar or complementary sensors.

In FY14, development will focus on further extending our natural user interface system to address the concurrent operation of manipulation and mobility aspects of hybrid robotic systems such as Robonaut 2 with legs (ground only in FY14) or an ATHLETE robot driving while manipulating a payload.

Human Robotic Systems (HRS): Controlling Robots over Time Delay Element
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This element involves the development of software that enables easier commanding of a wide range of NASA relevant robots through the Robot Application Programming Interface Delegate (RAPID) robot messaging system and infusing the developed software into flight projects.  In June and July of 2013, RAPID was tested on ISS as the robot messaging software for the Technology Demonstration Mission (TDM) Human Exploration Telerobotics (HET) Surface Telerobotics experiment.  RAPID has also been made available to — and integrated with — the Robot Operating System (ROS), a popular software framework for developing state-of-the-art robots for ground and space. While ROS powers a number of new robots and components such as Robonaut 2’s climbing legs and R5, the addition of RAPID allows these robots to interoperate in collaborative human-robot teams, safely and effectively over time-delayed communications links. The objective this year is to take this space-tested software and extend it to providing video streaming from remote robots and delivering this new capability to the Exploration Ground Data Systems (xGDS) area within HRS.  xGDS will then deliver its software to Science Mission Directorate (SMD) funded field tests to improve the technology readiness moving leading (potentially) to being used for the Lunar Prospector Mission ground data systems.  Success will involve delivering RAPID to xGDS and then xGDS supporting SMD field test.

The team is also developing algorithms for sensors capable of reconstructing remote worlds and efficiently shipping that remote environment back to earth using the RAPID robot messaging system.  This type of system could eventually lead to scientists on earth gain new insights as they are able to step into the remote world.  This sensor also has the ability to engage the public, bringing remote worlds back to earth.  During FY13, this task used science operations personnel from current SMD projects to objectively measure improvement in remote science target selection and decision-making based. The team continues to work with SMD projects to ensure that the technologies being developed are directly responsive to SMD project personnel needs. The objective of this work in FY14 is to expand the range of science operations tasks addressed by the technology, and to perform laboratory demonstrations for JPL/SMD stakeholders of the immersive visualization of data from a sensor using an SMD representative environment.

During 2014, the “Controlling Robots Over Time Delay” project element will develop two technologies:

  • Develop RAPID robot messaging for unified cross-center operations platform for TDM, xGDS, and CCSDS
  • Sensor Systems for the Construction of Immersive Virtual Environments
PHOENIX MARS ROBOTIC ARM 4 RDR DERIVED V1.0
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The Phoenix Robotic Arm Derived Data consists of Robotic Arm (RA) Scoop Tip position data and components of force exerted by the RA. Data are included for both the spacecraft RA and the Payload Interoperability Testbed (PIT) RA. These data are derived from raw RA telemetry data that are not archived in PDS due to ITAR restrictions.
PHOENIX MARS ROBOTIC ARM 4 RDR DERIVED V1.0
공공데이터포털
The Phoenix Robotic Arm Derived Data consists of Robotic Arm (RA) Scoop Tip position data and components of force exerted by the RA. Data are included for both the spacecraft RA and the Payload Interoperability Testbed (PIT) RA. These data are derived from raw RA telemetry data that are not archived in PDS due to ITAR restrictions.
PHOENIX MARS ROBOTIC ARM CAMERA 3 RADIOMETRIC SCI V1.0
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The Robotic Arm Camera (RAC) experiment on the Mars Phoenix Lander consists of one instrument component plus command electronics. This RAC Imaging Science RDR data set contains radiometric data from the Robotic Arm Camera (RAC).
PHOENIX MARS ROBOTIC ARM CAMERA 3 RADIOMETRIC OPS V1.0
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The Robotic Arm Camera (RAC) experiment on the Mars Phoenix Lander consists of one instrument component plus command electronics. This RAC Imaging Operations RDR data set contains radiometric data from the Robotic Arm Camera (RAC).
PHOENIX MARS ROBOTIC ARM CAMERA 4 LINEARIZED OPS V1.0
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The Robotic Arm Camera (RAC) experiment on the Mars Phoenix Lander consists of one instrument component plus command electronics. This RAC Imaging Operations RDR data set contains linearized data from the Robotic Arm Camera (RAC).
PHOENIX MARS ROBOTIC ARM CAMERA 4 LINEARIZED OPS V1.0
공공데이터포털
The Robotic Arm Camera (RAC) experiment on the Mars Phoenix Lander consists of one instrument component plus command electronics. This RAC Imaging Operations RDR data set contains linearized data from the Robotic Arm Camera (RAC).
PHOENIX MARS ROBOTIC ARM CAMERA 2 EDR VERSION 1.0
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The Robotic Arm Camera (RAC) experiment on the Mars Phoenix Lander consists of one instrument component plus command electronics. This RAC Imaging Operations EDR data set contains raw data from the Robotic Arm Camera (RAC).
PHOENIX MARS ROBOTIC ARM CAMERA 2 EDR VERSION 1.0
공공데이터포털
The Robotic Arm Camera (RAC) experiment on the Mars Phoenix Lander consists of one instrument component plus command electronics. This RAC Imaging Operations EDR data set contains raw data from the Robotic Arm Camera (RAC).