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ATHLETE
ATHLETE
ATHLETE
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ATHLETE with Tweel wheels, climbing a hill
Quarter-scale ATHLETE prototype, with its principal investigator Brian Wilcox

ATHLETE (All-Terrain Hex-Limbed Extra-Terrestrial Explorer) is a six-legged robotic lunar rover under development by the Jet Propulsion Laboratory (JPL). ATHLETE is a testbed for systems, and is designed for use on the Moon.[1]

The system is in development along with NASA's Johnson and Ames Centers, Stanford University and Boeing.[2] ATHLETE is designed, for maximum efficiency, to be able to both roll and walk over a wide range of terrains.[1]

Systems

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The project aims to develop a multi-purpose system capable of docking or mating with special-purpose devices including refueling stations, excavation implements and/or special end effectors. The legs have six degrees of freedom (6-DOF) for generalized robotic manipulation.[1] Each ATHLETE is intended to have a payload capacity of 450 kilograms (990 lb),[1] in Earth's gravity with the capability of docking multiple ATHLETE vehicles together to support larger loads.

The ATHLETE is much larger than robotic systems previously used and has a diameter of around 4 metres (13 ft) and a reach of around 6 metres (20 ft).[1] Even with this larger size the project has allowed the facility for multiple units to be stowed and docked compactly for launch into an annular ring. This would mean that many vehicles can be efficiently stacked around a main payload on a single lander.[1]

The six 6-DOF legs allow more capabilities than other robotic systems such as Sojourner or the Mars Exploration Rovers. These mean that the slopes it could climb would be up to 35° on solid surfaces and 25° on soft surfaces,[1] such as the soft deposits of dust found on the Moon. Plans are to develop the system's capability of travel over rougher terrain and to increase the speed of ATHLETE to 10 kilometres (6.2 mi) per hour, 100 times faster than the Spirit and Opportunity rovers.[1]

Goals

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The JPL is aiming for a 10-year life span,[1] and the capability for re-usable delivery vehicles would mean that the goal of "an affordable lunar-surface flight experiment that demonstrates this technology on the Moon and subsequently uses it as part of the Human Lunar Return campaign to perform the needed robotic or human vehicle functions on the lunar surface."[1]

ATHLETE's purpose is to support lunar exploration operations. One hypothetical mission scenario features a mobile, crewed "base" supported by ATHLETEs capable of traversing thousands of kilometers and setting down temporarily to study interesting features along the way.[3]

Future improvements

[edit]

Planning for the future of the ATHLETE includes the ability to scale difficult obstacles by means of employing a launchable/releasable grappling hook and line which it will use to haul itself up even vertical slopes. There are also plans to introduce provisions for voice and gesture commands from suited astronauts in proximity to the ATHLETE, the ability to self-deploy from their storage facilities and the capability for "autonomous footfall placement".[1] Work was also done to adapt the Tweel technology for use with the rover.

[edit]
  • The ATHLETE rover in a test facility at JPL
    The ATHLETE rover in a test facility at JPL
  • Rover with crew habitat
    Rover with crew habitat
  • Pair of rovers with habitats
    Pair of rovers with habitats
  • Front view of rover with habitat
    Front view of rover with habitat
  • ATHLETE rovers traverse the desert terrain adjacent to Dumont Dunes, California
    ATHLETE rovers traverse the desert terrain adjacent to Dumont Dunes, California

References

[edit]
[edit]
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ATHLETE

View on Grokipedia
from Grokipedia
ATHLETE, or All-Terrain Hex-Limbed Extra-Terrestrial Explorer, is a six-legged robotic rover concept developed by NASA's Jet Propulsion Laboratory (JPL) to support human exploration of the Moon and other extraterrestrial bodies. Designed as a heavy-lift utility vehicle, it features six limbs, each equipped with a wheel for rolling over stable terrain and capable of walking across soft, obstacle-laden, steep, or extreme surfaces, while also functioning as general-purpose manipulators for tasks like gripping, drilling, or scooping. The rover's primary purpose is to facilitate the unloading of bulky cargo from stationary landers, transport it over long distances, and enable operations on challenging environments, such as asteroid surfaces where it can absorb landing impacts using its limbs to minimize debris disturbance. ATHLETE's wheel-on-limb architecture allows for lighter overall mass compared to traditional planetary rovers by optimizing wheels for nominal terrain and relying on walking modes only when necessary, with each limb providing six degrees of freedom and powered by 1-horsepower motors. Development began under NASA's Exploration Technology Development Program, with prototypes tested from 2005 to 2012, including first-generation models weighing approximately 850 kg and capable of carrying 300 kg payloads in Earth gravity, and second-generation Tri-ATHLETE units that dock to form a six-limbed system with enhanced 450 kg payload capacity. Efforts concluded around 2012 with no further active development as of 2023. Demonstrations up to that time focused on cargo handling, low-gravity simulations using specialized testbeds, and integration of modular tools from a "tool belt" for versatile in-situ operations.

Overview and History

Development Background

The ATHLETE (All-Terrain Hex-Limbed Extra-Terrestrial Explorer) rover concept emerged as part of NASA's response to the challenges of lunar exploration outlined in the Vision for Space Exploration, announced in 2004, which emphasized the need for advanced mobility systems capable of traversing diverse and uneven terrain beyond the limitations of traditional wheeled rovers. This vision called for robotic precursors to support human return to the Moon, including site reconnaissance and resource utilization, prompting the development of versatile, multi-purpose vehicles to handle cargo transport and manipulation in rugged environments. Initial conceptualization at NASA's Jet Propulsion Laboratory (JPL) occurred between 2003 and 2005, drawing inspiration from prior legged robotics research to address the demands of extreme lunar topography. Engineers at JPL, building on earlier prototypes like the Limbed Excursion Mechanical Utility Robot (LEMUR)—a six-legged walker developed in the late 1990s for in-space assembly and utility tasks—envisioned a larger-scale system combining wheeled efficiency with legged adaptability. The wheel-on-limb design was formalized in early 2005, with hardware development commencing shortly thereafter, aiming to create a heavy-lift utility rover for unloading landers and transporting habitats over long distances. Primary development was led by JPL, under the management of NASA's Johnson Space Center (JSC) as part of the Human-Robot Systems (HRS) Project within the Exploration Technology Development Program. Funding came from the NASA Exploration Systems Mission Directorate, supporting rapid prototyping and field testing to align with lunar outpost goals. This collaboration integrated JPL's robotics expertise with JSC's human exploration focus, evolving the concept from small-scale legged platforms like LEMUR into a scalable system for planetary surfaces.

Key Milestones

The development of ATHLETE commenced in 2005 with the construction and demonstration of its first prototype at NASA's Jet Propulsion Laboratory (JPL), where the robot showcased basic hexapod walking on simulated extraterrestrial terrain. This 850 kg prototype, featuring six limbs each with six degrees of freedom, marked the initial proof-of-concept for wheel-on-limb mobility, enabling both walking and rolling gaits. In 2008, ATHLETE underwent integration with the Chariot rover platform during hybrid mobility tests as part of joint field operations, demonstrating coordinated transport and navigation capabilities in challenging environments. These experiments, conducted at the Moses Lake sand dunes in Washington—a lunar analog site—evaluated multi-asset collaboration, including long-distance drives and terrain interaction. From 2010 to 2012, scale-model variants of ATHLETE, including the half-scale Tri-ATHLETE configuration constructed in 2009, were tested in lunar analog sites such as Moses Lake, Washington, and the Black Point Lava Flow in Arizona, with a focus on regolith handling and stable locomotion in loose, uneven soils. These trials, part of NASA's Desert Research and Technology Studies (DRATS), validated the system's ability to manage soil displacement and maintain footing during walking and wheeling modes, informing refinements for planetary surface operations. In 2012, a low-gravity testbed was developed to simulate ATHLETE operations on asteroids and small bodies, using suspension systems to replicate reduced gravity environments and test landing impact absorption. Active development concluded around 2012 following restructuring of NASA's exploration programs. Key publications advanced the technical understanding of ATHLETE, including a 2006 IEEE paper detailing the limb mechanics and motion planning for efficient hexapod traversal. Additionally, a 2012 conference paper explored multi-rover coordination strategies, emphasizing collaborative cargo handling and navigation for exploration missions.

Design and Systems

Mobility and Locomotion

The ATHLETE rover employs a hexapod architecture with six articulated limbs, each providing six degrees of freedom (DOF) through a serial kinematic chain consisting of a hip yaw joint, hip pitch joint, knee pitch joint, knee roll joint, ankle pitch joint, and ankle roll joint, augmented by a seventh DOF from the wheel at the limb's end effector. The prototype uses Michelin Tweel non-pneumatic wheels (0.5 m diameter) for compliance, while second-generation employs Michelin Lunar Wheels (71 cm diameter, supporting up to 4500 N). This wheel-on-limb configuration enables seamless transitions between rolling and walking gaits, optimizing energy efficiency and terrain traversal. The limbs' design supports not only locomotion but also manipulation tasks, with the wheel capable of locking to function as a foot during walking. Locomotion modes include wheeled traversal for efficient movement on flat or gently rolling terrain, achieving speeds up to 10 km/h via powered wheel actuation and active suspension that distributes forces evenly across the limbs to maintain a level body pose. In legged walking mode, the locked wheels serve as contact points for navigating steep terrain; for slopes exceeding 20 degrees, a rappelling mode using a winch enables descent where wheeled systems would fail. Additionally, the multi-limbed structure provides self-righting capability through coordinated repositioning of unused limbs to recover from tip-overs or uneven settling. The rover's terrain adaptability stems from its ability to step over obstacles nearly equal to its fully extended limb length—approximately 1.8 meters for the prototype—and to straddle or navigate around craters up to 1 meter in depth by adjusting limb poses. Load distribution across the six limbs prevents excessive sinkage in loose regolith, with ground pressures ranging from 20 to 45 kPa, supporting payloads up to 450 kg in Earth gravity for the second-generation prototype. This is facilitated by force-torque sensing at the limb ends and algorithmic control for even weight sharing. Limb coordination for these capabilities relies on forward and inverse kinematics models to compute the end-effector pose from joint angles, enabling precise planning of foot placements and body leveling during both rolling and walking, with a limb length of approximately 1.8 meters from hip to wheel center.

Power and Control Systems

The ATHLETE rover's power system centers on a 60V DC power bus that distributes energy to its actuators, cameras, and computing resources, with a separate 12V auxiliary line for low-power components. Primary energy storage consists of four Valence Technologies lithium iron magnesium phosphate batteries connected in series, forming a 78 kg pack rated at 51.2 V and 130 Ah capacity, capable of delivering up to 300 A for 30 seconds to support peak loads during mobility or manipulation tasks. These batteries are recharged via a pair of 1 kW/60 V power supplies, managed by an integrated battery management system that monitors voltage, current, temperature, and state of charge to optimize performance and prevent over-discharge. In mission concepts for shadowed lunar or planetary environments, radioisotope thermoelectric generators (RTGs) have been considered as supplementary power sources to extend operational endurance beyond solar-dependent recharging, though prototypes primarily rely on battery systems for testing. Control architecture employs a hierarchical structure with a central main processor housed in the rover body, which issues high-level commands for coordinated limb motion and closed-chain posing across the six limbs. This processor communicates with distributed motor controllers—co-located at each actuator—over a CAN bus (in second-generation prototypes), enabling real-time execution of position control loops at 2.7 kHz per joint. Onboard computing utilizes a rack of four 800 MHz PowerPC-based XCalibur 1000 cards in a cPCI enclosure, with dedicated nodes for motion coordination, ground communication, and stereo vision processing from up to 24 cameras; this distributed setup facilitates fault-tolerant operation by isolating processing tasks and allowing limb-level redundancy in case of failures. While specific operating systems are not detailed in prototype documentation, the system's design supports deterministic real-time performance essential for gait planning and stability maintenance during traversal. Autonomy capabilities are augmented by the ground-based FootFall Planning System, which generates collision-free paths for limb placements using single-query bi-directional (SBL) sampling planners combined with terrain mapping from stereo-derived digital elevation models (DEMs). These algorithms incorporate lazy collision detection via bounding volume hierarchies and post-process paths with Dijkstra's shortest-path optimization for smoothness, ensuring static stability by keeping the center of gravity within the support polygon on slopes up to 14°. Fault-tolerant software monitors joint torques—derived from encoder data and stiffness models—to detect overloads and trigger safeguards like motion halts or limb adjustments, complemented by hardware features such as harmonic drive fuses and power-off brakes for mechanical redundancy. In cooperative modes with multiple ATHLETE units, queued commands synchronize actions while continuously verifying force bounds to prevent damage. Energy efficiency is achieved through the wheel-on-limb design, which sizes actuators for typical terrain (120 W brushless DC motors for joints, 746 W for wheels) rather than extreme cases, yielding mass savings that offset the articulated structure's added weight compared to wheeled chassis. This enables wheeled-mode traversal at up to 10 km/h with energy draws optimized for nominal loads, while legged modes reserve higher power for obstacles, supporting 300–450 kg payloads over extended field tests totaling more than 6 km. Algorithms for load distribution and torque minimization further reduce consumption, with sway-gait planning demonstrated to improve torque margins by over 20% during walking, though specific Wh/km figures vary by terrain and configuration.

Scientific Instruments

The ATHLETE rover incorporates a suite of core sensors to support terrain navigation and environmental assessment during exploration tasks. Multiple pairs of stereo cameras, positioned along the hexagonal frame and limbs, enable 3D terrain reconstruction and hazard detection by processing visual data into depth maps. For instance, each face of the frame features a stereo camera pair, contributing to a total of up to 48 cameras in advanced configurations for comprehensive 360-degree coverage and underbody viewing. Additionally, high-resolution tilt sensors and a MEMS inertial measurement unit (IMU) provide inclinometer-like functionality to measure vehicle attitude and assess slope stability, ensuring safe traversal over uneven lunar or planetary surfaces. ATHLETE's modular payload bay, often configured as a structural pallet or drop tray, accommodates diverse scientific tools and supports in-situ resource utilization (ISRU) activities. This bay can carry up to 450 kg of payload in Earth gravity, including sample manipulators such as grippers and scoops for collecting regolith or positioning cargo. Limb-mounted interfaces allow attachment of tools like augers or backhoes directly to the wheel hubs, enabling excavation and material handling without requiring the entire rover to reposition, a key advantage for precise sampling in constrained terrains. Demonstrations have shown these tools excavating soil or deploying drills on vertical surfaces, facilitating ISRU tasks like resource prospecting. While specific spectrometers such as visible-near infrared (VNIR) units are not integrated as standard, the modular design permits hosting third-party instruments for mineralogical analysis. Data handling on ATHLETE emphasizes real-time processing of sensor inputs, with up to four onboard PowerPC computers dedicated to stereo vision and navigation algorithms. These systems manage video streams from limb-end and frame cameras via Ethernet connections, supporting safeguarded teleoperation and basic autonomy for instrument deployment. Force-torque sensors in the limbs further enhance data accuracy by detecting contact forces during tool operations, contributing to reliable environmental interaction.

Mission Goals and Capabilities

Exploration Objectives

The ATHLETE rover was designed to enable resource prospecting in challenging lunar environments, particularly targeting water ice deposits in the permanently shadowed craters at the lunar south pole, through the use of interchangeable limb-based tools such as auger drills and scoops for soil sampling and resource collection. Its primary goals also include conducting long-range traverses across rugged terrain for landing site reconnaissance and natural resource analysis, supporting unmanned precursor missions to reduce risks for future human exploration. These objectives position ATHLETE as a versatile platform capable of traversing obstacles up to 1.8 meters in height—nearly its full limb extension—and more than three times its wheel diameter, allowing access to areas inaccessible to traditional wheeled rovers. Secondary objectives focus on facilitating human-robotic precursor missions by delivering cargo from landers to outposts, setting up habitats, and enabling in-situ construction of lunar infrastructure, such as assembling and maintaining assets using its six multi-degree-of-freedom limbs as manipulators. With a payload capacity of up to 450 kg in lunar-scale prototypes and the ability to dock multiple units for cooperative tasks, ATHLETE supports logistical operations like relocating crew modules and transporting bulky equipment over distances at speeds up to 10 km/h in rolling mode. This enhances efficiency in precursor activities, including technology demonstrations for sustained surface operations. Compared to wheeled rovers, ATHLETE offers superior mobility with active suspension for maintaining level pose on uneven surfaces and the option to transition from rolling on benign terrain to walking on steep or soft regolith, potentially improving energy efficiency through distributed control and lightweight wheel-on-limb design. NASA studies highlighted its rappelling capabilities for slopes greater than 20 degrees to offload weight and improve performance on steep terrain. These advantages stem from its hexapod architecture, which briefly references advanced locomotion modes detailed elsewhere. ATHLETE's objectives align with NASA's broader vision for sustainable lunar presence, as outlined in early 21st-century exploration architectures under the Exploration Systems Mission Directorate. Development of prototypes occurred from 2005 to 2012, with no flight missions as of 2023.

Operational Scenarios

ATHLETE operational scenarios encompass a range of mission contexts, from lunar exploration to planetary analogs, leveraging its hex-limbed design for versatile mobility and manipulation. These scenarios emphasize the rover's ability to navigate challenging terrains, coordinate with other assets, and mitigate environmental risks while supporting scientific objectives. In lunar applications, ATHLETE is conceptualized for traversing the rim of Shackleton Crater near the Moon's South Pole, a region of interest for its permanently shadowed areas potentially containing water ice. A notional mission involves robotic precursors establishing a base on the crater rim, followed by ATHLETE-led traverses to multiple sites for geological sampling and instrument deployment. Over approximately 28 days, the rover could support exploration of 15-20 distinct locations along ridges, massifs, and crater chains, deploying science packages such as seismometers and heat probes at key points like the Malapert Massif ridge. This enables systematic coverage of impact materials from various lunar epochs, facilitating studies of crustal structure and resource utilization. Hybrid operations integrate ATHLETE with wheeled rovers, enhancing mission flexibility through physical docking for cargo transfer. Tri-ATHLETE variants, consisting of two three-limbed units, dock via hook-and-pin interfaces on structural pallets to form a six-limbed system capable of offloading and transporting up to 500 kg payloads from lander decks up to 3.2 m high. This allows seamless cargo handover to wheeled assets for faster traversal on benign terrain, with undocking enabling independent mobility; such coordination supports outpost construction or sample logistics without dedicated power sharing mechanisms. Risk mitigation protocols address lunar and planetary hazards like dust accumulation and thermal extremes ranging from -150°C to 120°C. For dust, ATHLETE employs non-pneumatic wheels with deformable designs for flotation in loose regolith, transitioning to walking mode if sinking occurs, and uses titanium-band wheels resistant to degradation from outgassing or UV exposure. Thermal management incorporates actuators and materials rated for 40-400 K extremes, with onboard autonomy for hazard avoidance during unpowered phases; these features ensure operational reliability in shadowed craters or diurnal cycles.

Testing and Future Prospects

Field Tests and Demonstrations

The All-Terrain Hex-Limbed Extra-Terrestrial Explorer (ATHLETE) prototypes underwent several field tests in analog environments to validate their mobility, walking capabilities, and operational reliability in terrains simulating lunar or planetary surfaces. These tests focused on long-distance traverses, slope navigation, and integration with other systems, providing critical data for design refinements. A significant demonstration occurred during the 2008 integrated field test at Moses Lake Sand Dunes, Washington, spanning two weeks under NASA's Human Robotic Systems Project. There, first-generation ATHLETE prototypes (SDM-B models) performed extended traverses, docking maneuvers with habitat mockups, and navigation over steep slopes up to 14 degrees, while employing the FootFall Planning System for obstacle avoidance and single-step walking. The tests exposed challenges such as chassis sagging due to wheel compliance in soft sand (up to 20 cm under load) and limitations in terrain visibility from onboard cameras, but successfully validated collision-free motion planning and safe stepping over rocks, achieving reliable operations despite environmental stressors like rain and sandstorms. In September 2010, ATHLETE participated in the Desert Research and Technology Studies (Desert RATS) at Black Point Lava Flow, Arizona, a volcanic analog site mimicking lunar regolith and rocky terrain. Over a 14-day expedition, second-generation prototypes (a coordinated pair of Tri-ATHLETE vehicles docked to a central cargo pallet simulating a habitat) covered approximately 40 km while executing full gait cycles in discontinuous reverse wave sequences to navigate large obstacles. Key outcomes included successful open-loop walking that advanced the chassis by about one-third of its body length per cycle, with a compliance model accurately predicting sags (average error of 0.9 cm) to maintain ground clearance; image processing effectively segmented self-imaged limbs from terrain models in most cases, though shadows posed occasional issues. These results demonstrated high operational uptime in regolith-like conditions and informed upgrades to torque telemetry and planning heuristics for future iterations. Analog sites like the Arizona lava fields proved ideal for slope testing, where ATHLETE's limb-based locomotion handled uneven, rocky inclines representative of extraterrestrial challenges, highlighting the system's versatility over wheeled alternatives in such environments. Early lab milestones, such as compliance modeling at JPL's Mars Yard, directly supported these field successes by enabling predictive adjustments for real-world deformations.

Proposed Missions and Improvements

ATHLETE has been proposed for integration into future NASA missions as a versatile heavy-lift rover capable of supporting human exploration on the lunar surface, particularly in unloading cargo from stationary landers and transporting payloads over long distances across varied terrain. In the context of the Artemis program, a high-capacity variant of ATHLETE is conceptualized as a multi-limbed mobility platform for offloading habitats and large payloads from high-decked landers, enabling precision placement and construction tasks at lunar outposts. This design leverages modular assembly, where individual limbs can be delivered separately and combined into self-driving configurations like Tri-ATHLETE units, facilitating stepped payload capacities in lunar gravity. Ongoing improvements focus on enhancing ATHLETE's modularity and functionality to better suit extended missions. The second-generation Tri-ATHLETE prototype introduces cooperative three-limbed robots that dock to form a six-limbed system, with quick-disconnect end effectors allowing limbs to serve as general-purpose manipulators equipped with tools such as drills, grippers, or scooping devices powered by onboard motors. Further advancements include cross-cabled, winch-tendon four-bar frames for limbs, enabling hot-swapping for maintenance and independent operation as cranes, which reduces overall system mass by optimizing wheels for nominal terrain while reserving walking modes for extremes. These upgrades aim to support in-situ resource utilization tasks, such as excavation and 3D printing, though integration with additive manufacturing for on-site repairs remains under exploration in conceptual studies. In 2022–2023, a Small Business Innovation Research (SBIR) project by Astroport Space Technologies adapted an ATHLETE-based platform for lunar surface site preparation, including construction of landing/launch pads and blast shields using in-situ regolith. This system supports Artemis missions by enabling autonomous infrastructure development, with the project advancing to Phase II in 2024. Key challenges for ATHLETE's deployment include achieving cost-effective production, as early prototypes exceeded $2 million each, scaling to full units potentially in the tens of millions while maintaining robustness for uncrewed operations. Radiation hardening is critical for long-duration missions in space environments, requiring advanced shielding without compromising mobility, alongside simulations for low-gravity behaviors to mitigate issues like terrain instability on sloped or soft surfaces. As of 2023, JPL and partners continue to refine ATHLETE concepts for Artemis-era lunar logistics, with studies emphasizing multi-vehicle coordination for habitat assembly, though no selections for specific missions like VIPER have been confirmed.

References

  1. https://www-robotics.jpl.nasa.gov/how-we-do-it/systems/the-athlete-rover/
  2. https://www.nasa.gov/image-article/athlete/
  3. https://www.nasa.gov/wp-content/uploads/2023/01/55583main_vision_space_exploration2.pdf
  4. https://ntrs.nasa.gov/citations/20040041363
  5. https://www-robotics.jpl.nasa.gov/media/documents/LEMUR_AR.pdf
  6. https://www-robotics.jpl.nasa.gov/media/documents/ATHLETE_iSAIRAS_2008.pdf
  7. https://www-robotics.jpl.nasa.gov/media/documents/2469684volpe.pdf
  8. https://robotics.jpl.nasa.gov/media/documents/Heverly_2010_AMS_Tri-ATHLETE.pdf
  9. https://ieeexplore.ieee.org/document/4839635/
  10. https://www2.ccs.neu.edu/research/gpc/publications/Mittman_Norris_Powell_Torres_McQuin_Vona__2008__Lessons_Learned_from_All-Terrain_Hex-Limbed_Extra-Terrestrial_Explorer_Robot_Field_Test_Operations_at_Moses_Lake_Sand_Dunes_Washington.pdf
  11. https://ntrs.nasa.gov/api/citations/20100021930/downloads/20100021930.pdf
  12. https://onlinelibrary.wiley.com/doi/abs/10.1002/rob.20410
  13. https://motion.cs.illinois.edu/papers/Hauser-2006-Athlete.pdf
  14. https://www.semanticscholar.org/paper/ATHLETE%3A-A-limbed-vehicle-for-solar-system-Wilcox/bf81662a1fa70db456a866962ed90fd1c7abf15c
  15. https://www-robotics.jpl.nasa.gov/media/documents/Heverly_2010_AMS_Tri-ATHLETE.pdf
  16. https://ntrs.nasa.gov/api/citations/20110016533/downloads/20110016533.pdf
  17. https://www.popsci.com/technology/article/2013-01/meet-athlete-nasas-robot-moon-walker/
  18. https://ntrs.nasa.gov/api/citations/20140008625/downloads/20140008625.pdf
  19. https://www.lpi.usra.edu/science/kring/lunar_exploration/Shackleton-Malapert.pdf
  20. https://www.jpl.nasa.gov/news/athlete-rover-steps-up-to-long-desert-trek/
  21. https://ntrs.nasa.gov/citations/20220001545
  22. https://techport.nasa.gov/projects/125628
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