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Robotics Technology Development at Ames 20 HET Teleroboc Systems Robonaut 2 Humanoid robot (42 DOF, human-scale/safe) Perform dexterous IVA/EVA manipulaon tasks Share astronaut tools and workspaces Smart SPHERES Free-flyi ng robot (6 axis, cold-gas propulsion) Perform IVA/EVA remote mobile sensor tasks Improve ground control situaon awa r enes s Surface Telerobocs Mobile robot on surface (Moon, asteroid, Mars) Perform surface acvi es before/support/aer crew Crew centric operaons from inside flight vehi cl e PDF created with pdfFactory trial version www.pdffactory.com

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Robotics Technology Development at Ames 20

HET Telerobo c Systems

Robonaut 2• Humanoid robot(42 DOF, human-scale/safe)

• Perform dexterous IVA/EVA manipula on tasks

• Share astronaut tools and workspaces

Smart SPHERES• Free-flyi ng robot (6 axis, cold-gas propulsion)

• Perform IVA/EVA remote mobile sensor tasks

• Improve ground control situa on awa reness

Surface Telerobo cs • Mobile robot on surface(Moon, asteroid, Mars)

• Perform surface ac vi es before/support/a er crew

• Crew centric opera ons from inside flight vehi cl e

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Robotics Technology Development at Ames 21

Surface Telerobo cs

Candidate Missions• L2 Lunar Farside. Orion crew module test flight (~2020) to Ear th- Mo on L2 poi nt

• Near-Earth Asteroid. NEA dynamics and distance make it impossible to manually control robot from Earth

• Mars Orbit. Crew must operate surface robot from orbit when circumstances (con ngency, et c. ) pr ecl ude Ear th cont rol

What will the test achieve?• Obtain baseline engineering data• Validate & correlate prior ground simula ons • Reduce the risk that mission planning is based on inaccurate assump ons

Surface Telerobo cs is an engineering test of a human-robot “opscon” for future deep-space human explora on mi ssi ons

(NASA GSFC)

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Robotics Technology Development at Ames 22

L2 Lunar Farside (Waypoint) Mission Concept

Orion at Earth-Moon L2 Lagrange point• 60,000 km beyond lunar farside• Allows sta on keepi ng wi th mi ni ma l fuel • Crew remotely operates robot on lunar

farside• Less expensive than human surface mission• Does not require human-rated lander

Primary objec ve: lunar tel escope • Use telerobo o set up radi o tel escope • Requires surface survey, antenna/receiver

deployment, and inspec on/docume nt a on • Lunar farside provides radio quiet zone for

low-freq measurements cosmic dawn

Secondary objec ve: samp l e col lec on • Use telerobo o per form field geol ogy • Requires scou ng, samp l ing (pos si bl y

subsurface), and sample caching/return• South Pole Aitken (SPA) basin sampling is

the highest priority lunar science objec ve

(Lockheed Martin / LUNAR)

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Robotics Technology Development at Ames 23

Waypoint Mission Simula on (2013)

June 17 July 26 August 20Spring 2013

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Robotics Technology Development at Ames 24

Crew Interface (Task Sequence Mode)

Terrain hazardsTerrain hazards

Task Sequence

Task Sequence

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Robotics Technology Development at Ames 25

Crew Interface (Teleop Mode)

Rover pathRover path

Motion

controls

Motion

controls

Terrain hazardsTerrain hazards Rover cameradisplay

Rover cameradisplay

Camera

controls

Camera

controls

3D View controls3D View controls

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Robotics Technology Development at Ames 26

“Live” Rover Sensor and Instrument

Data (telemetry)

Crew Interface on SSC

K10 rover at NASA Ames

Data Communica ons (Ups i de- down Payl oad)

384 kbits/sec (min), 5 sec delay (max)Uplink

8 kbits/sec (min), 5 sec delay (max)

Downlink

384 kbits/sec (min), Out-of-Band

Uplink, data transferto laptop storage

Rover Task Sequence (text file)

Interface Instrumenta on & Evalua on Da ta

Post-test File Transfer

Rover/Science Data (e.g. imagery)

Note: Normal uplink ~1Mbps, spike a er LOS is ~2Mbps for 2 sec

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Robotics Technology Development at Ames 27

K10 rover before dawn in the ARC “Roverscape”

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Robotics Technology Development at Ames 28

K10 Planetary Rover @ NASA Ames

NASA Ames Roverscape

K10 Specifications• 4-wheel drive, 4-wheel steer• Split rocker chassis• Size: 1.3 x 0.9 x 1.0 m (HxWxL)• Speed: 0.9 m/s (on 10 deg slope)• Power: 1900 W (Li-ion batteries)• Weight: 100 kg (with 25 kg payload)

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Robotics Technology Development at Ames 29

Telerobo cL unar Tel escope Depl oyme nt

K10 deploying simulated polyimide antenna.

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Robotics Technology Development at Ames 30

K10 Deploys Kapton Film in Marscape

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Robotics Technology Development at Ames 31

Chris Cassidy uses the “Surface Telerobo cs Wo r kbench”

Astronaut remotely operates K10 from the ISS (2013-06-17)

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Robotics Technology Development at Ames 32

Astronauts Parmitano & Nyberg Operate K10 from ISS

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Robotics Technology Development at Ames 33

ISS Mission Control (MCC-H) during Surface Telerobo cs test (2013- 08- 20)

View of Karen Nyberg using robot interface (top center) and K10 at ARC (top le )

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Robotics Technology Development at Ames 34

“PLUTO” Mul -Pur pose Suppor t Room at JSC

Provides data comm & crew laptop support

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Robotics Technology Development at Ames 35

Mul -Mi ssi on Oper a ons Cent er (MMO C ) at ARC

Manages Surface Telerobo cs test sessi ons

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Robotics Technology Development at Ames 36

K10 support team at ARC

Provides rover engineering & test logis cs

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Robotics Technology Development at Ames 37

Ques ons?

Intelligent Robo cs Gr oup Intelligent Systems DivisionNASA Ames Research Center

irg.arc.nasa.gov

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