SherpaTT


Technical Details

Size: Variable, smallest foot print: 1m x 1m. Biggest foot print: 2.4m x 2.4m. Height ranges from 0.8m to 1.8m
Weight: 150 kg
Power supply:
LiPo primary battery: 44,4 V; 10 Ah & LiPosecondary battery: 44,4 V; 10 Ah (autonomous hot switching)
Speed: 0.7 m/s (max) 0.1 m/s (nominal)
Actuation/ Engine:
4-wheel drive with active ground adaption, alternatively short traverses of walking motion
Sensors:
- Lidar: Velodyne HDL-32E
- Laser range finder: Hokuyo UST-20LX
- Camera: Basler Ace (2048 x 2048px, 25 fps)
- IMU: Xsens MTi-300 AHRS
- Force-Torque sensor FT-DELTA 160 at each wheel
Communication:
- Mobile access point: 2.4 GHz, 802.11n,
- Remote control: Bluetooth
- Remote stop: 868 MHz Xbee-Pro
On-Board Computer:
IntelCore i7-4785T, 2.2GHz
Structure and Mechanisms:
- 6 DoF Manipulator
- 4x 5DoF Suspension Units

Organisational Details

Sponsor: Federal Ministry for Economic Affairs and Climate Action
German Aerospace Center e.V.
Grant number: Grant no. 50 RA 1301
Application Field: Space Robotics
SAR- & Security Robotics
Underwater Robotics
Related Projects: FT-Utah
Field Trials Utah with the TransTerrA System (06.2016- 03.2017)
SIROM (OG5)
Standard Interface for Robotic Manipulation of Payloads in Future Space Missions (11.2016- 02.2019)
ROBDEKON
Robot systems for decontamination in hostile environments (06.2018- 06.2022)
ADE (OG10)
Autonomous Decision Making in Very Long Traverses (02.2019- 04.2021)
Skylight
Tethered Micro Rover for Safe Semi-Autonomous Exploration of Lava Tubes (07.2020- 10.2020)
RoBivaL
Robot Soil Interaction Evaluation in Agriculture (08.2021- 07.2023)
TransTerrA
Semi-autonomous cooperative exploration of planetary surfaces including the installation of a logistic chain as well as consideration of the terrestrial applicability of individual aspects (05.2013- 12.2017)
Related Robots: Sherpa
Expandable Rover for Planetary Applications
Coyote III

System description

SherpaTT in the artifical crater environment of DFKI RIC (Photo: Florian Cordes, DFKI)
SherpaTT, equipped with final hull oft he central body and flexible wheels in the artifical crater environment of DFKI RIC (Photo: Florian Cordes, DFKI)
CAD-Rendering of the underwater version SherpaUW (Rendering: David Grünwald, DFKI)
SherpaTT is a hybrid walking and driving rover with an active suspension system developed for high mobility in irregular terrain. The internal power supply (2x 10,000m Ah@44.4 V), a lidar sensor, a camera and the manipulator arm allow the cinduction of autonomous exploration activities.

The rover is equipped with six standardized electro-mechanical interfaces, one of them being the manipulators hand interface. Due to the electro-mechanical itnerfaces, the robot can be equipped and reconfigured with modular payload items to match the current task. One example being the usage of modular sampling devices, that can be sealed and handed over to the robotic team mate Coyote III.

SherpaTT’s overall weight is about 150 kg. Due to self-locking gears in the four suspension units, the rover is able to cope with high additional payload weights without increasing energy consumption to maintain the current robot’s body pose.

SherpaTT is developed within the scope of the project TransTerrA which aims to implement a logistics chain, based on a heterogeneous team of mobile and stationary robotic devices. SherpaTT has the role of an exploration and sample collecting rover in the heterogeneous robotic team. Collected samples are handed over to the Shuttle rover (Coyote III) for transport to the landing site and eventually sample return to earth.

SherpaTT represents an enhanced design of the Sherpa rover, which was originally developed within the RIMRES project. The design considerations and development concept of SherpaTT is derived from the lessons learned of Sherpa.  By introducing a knee joint within the suspension units (“legs” of the system, a three dimensional workspace is created. Furthermore two of the joints in the original design were used very rarely. Hence, a reduction from six degrees of freedom (DoF) in the original design to five  DoF in the new design along with a significant increase of the workspace of each suspension unit was possible.

Besides the primary scenario with respect to extraterrestrial exploration, SherpaTT demonstrates its application to terrestrial scenarios as well, such as search and rescue and /or security. The water proof design of the suspension units allows to exchange the central body of the robot to create SherpaUW which is aspired to be applied in deep sea exploration scenarios.

Videos

Field Trials Utah: Robot team simulates Mars mission in Utah

A barren, rocky desert landscape and not a single soul around – to come as close as possible to the inhospitable conditions on the Red Planet, scientists of the Robotics Innovation Center of the German Research Center for Artificial Intelligence (DFKI) tested the cooperation of various robot systems in the desert of the American state of Utah from 24 October to 18 November 2016.

SherpaTT: Driving in natural Mars analogue terrain in the desert of Utah, US

SherpaTT driving in natural Mars analogue terrain in the desert of Utah, USA and demonstrating its ability to keep its body level during drives through rough terrain.

SherpaTT during outdoor runs

SherpaTT demonstrating its ability to keep ist body level during drives through rough terrain.

Field Trials Morocco: EU partner test new software with DFKI rover SherpaTT

The objective of the Strategic Research Cluster (SRC) on Space Robotics Technologies funded by the European Union is to enable major advances in space robotic technologies. Among others, these technologies are needed for future robotic missions to explore the surfaces of Mars, Moon and other celestial bodies. At the first stage of the SRC implementation (2016–2019), several research & development projects ("operational grants") established core technologies for space robotic systems. Since lab environments cannot adequately simulate the harsh environmental conditions a space exploration robot will be confronted with, field tests in terrestrial Mars or Moon analogues are imperative.

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last updated 22.08.2023
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