Space robotics
DraftRobots do the work in space that crews cannot afford to do and cannot reach. The engineering is shaped by three constraints absent on Earth: no gravity to react against, no opportunity for repair, and a control loop that may take minutes to close.
Manipulators
A robotic arm on Earth pushes against a floor bolted to a planet. In orbit, the arm and the spacecraft form one dynamical system, and moving the arm moves the spacecraft.
| Consequence | Effect |
|---|---|
| Reaction torque | Arm motion imparts equal and opposite motion to the base |
| Coupled dynamics | The controller must model arm and base together, not the arm alone |
| Attitude interaction | Attitude control fights the arm unless the two are coordinated |
| Momentum management | Repeated motions accumulate momentum in the reaction wheels |
The flown solutions are large and slow. Canadarm and Canadarm2 move deliberately, with the station’s attitude control coordinated against planned arm motion. Canadarm2 can also relocate itself end over end between grapple fixtures on the station’s exterior, effectively walking, which extends its reach far beyond its length.
The Mission Extension Vehicle demonstrated the commercial case for manipulation without actually manipulating much. Rather than repairing or refuelling a satellite, it docks to the target’s apogee engine nozzle, a structure present on nearly every geostationary satellite, and then provides attitude control and station keeping using its own propulsion. It is a deliberately minimal approach that avoids the hard problems, and it works. See In-space manufacturing and assembly.
Surface rovers
| Rover | Mission duration | Total traverse |
|---|---|---|
| Sojourner, 1997 | 83 days | ~100 m |
| Spirit, 2004 to 2010 | 6 years | 7.7 km |
| Opportunity, 2004 to 2018 | 14 years | 45 km |
| Curiosity, 2012 onward | Ongoing | Over 30 km |
| Perseverance, 2021 onward | Ongoing | Over 30 km |
| Yutu-2, 2019 onward | Ongoing | Lunar far side |
Mars rover driving is constrained by the communication cycle rather than by speed. A traverse is planned on the ground from the previous day’s imagery, uplinked, and executed. The rover then waits for the next cycle. Even with autonomous navigation, which lets a rover assess terrain and pick a path itself, throughput is limited to roughly one command cycle per sol.
Autonomous navigation builds a terrain model from stereo imagery, evaluates traversability, and plans a path. Its value is measured directly in metres per sol: it lets a rover drive beyond what the operators could see when they planned, which multiplies daily progress.
Slip is the persistent problem. Wheels turn without the rover moving on loose regolith, which is why visual odometry is essential rather than supplementary. See Computer vision in space.
Wheel design has proved harder than expected. Curiosity’s thin aluminium wheels sustained significant damage from sharp embedded rocks earlier than predicted, requiring route planning to avoid certain terrain and a change in driving technique. Perseverance’s wheels were redesigned as a direct result.
Free flyers
Small robots that fly inside or around a spacecraft.
Astrobee and its predecessor SPHERES operate inside the ISS, using fans for propulsion and vision for navigation. Their value is routine work: inventory audits, camera work and sensor surveys that would otherwise consume crew time, which is the scarcest resource on a station.
External inspection free flyers can survey a spacecraft’s exterior for damage, which is otherwise only possible by EVA or by another spacecraft. The difficulty is that anything flying near a spacecraft is a collision risk, so proximity operations require the same care described in Rendezvous and docking.
Teleoperation under delay
Direct teleoperation degrades badly with delay. Above roughly a second of round trip, an operator controlling a manipulator directly will overshoot and oscillate, because the feedback arrives after the correction has been applied.
Predictive display helps in the intermediate range by showing the operator a simulated result of their command immediately, with the actual telemetry arriving later to correct the model. It works when the model is good, which means when the environment is well characterised.
At Mars delays, direct control is impossible and the only workable mode is supervised autonomy: the ground specifies a goal and the robot achieves it, with the ground reviewing the result a cycle later. This makes robot capability the throughput limit, which is why rover autonomy translates so directly into science return.
The unsolved problem
Grappling an uncooperative target remains beyond operational capability, and it is the enabling technology for both active debris removal and servicing the existing satellite fleet.
| Difficulty | Why |
|---|---|
| No grapple fixture | The target was never designed to be captured |
| Tumbling | Rotation, often about a changing axis, must be matched or absorbed |
| Unknown mass properties | Inertia and centre of mass are not known, so post-capture control is uncertain |
| Fragile structures | Solar arrays and antennas break, creating debris rather than removing it |
| Lighting | Point-source illumination with absolute shadows defeats many vision algorithms |
| One attempt | A failed capture may impart tumble, worsening the situation |
Approaches under development include robotic arms with vision-guided grasping, nets, harpoons, and adhesive or electrostatic capture. Each has failure modes that risk generating debris, which is the outcome the mission exists to prevent.
Demonstrations have made real progress. RemoveDEBRIS tested net and harpoon capture on deployed targets, Astroscale’s ELSA-d demonstrated magnetic capture of a prepared client, and ADRAS-J performed close approach and inspection of an actual derelict upper stage. All are proving technology rather than operating a service. See Space debris and traffic management.
Design constraints
| Constraint | Consequence |
|---|---|
| No repair | Mechanisms must survive the mission without maintenance |
| Vacuum | No conventional lubricants; cold welding risk; heat only leaves by radiation |
| Thermal cycling | Joints and actuators expand and contract every orbit |
| Dust | On the Moon and Mars, abrasive dust attacks seals and bearings |
| Radiation | Motor controllers and sensors need the tolerance described in Avionics |
| Mass | Every actuator, gearbox and structural element competes with payload |
Lubrication is the underappreciated one. Liquid lubricants evaporate and creep in vacuum, so space mechanisms use low-vapour-pressure oils in sealed or labyrinth arrangements, or solid lubricants such as molybdenum disulfide. Getting this wrong produces a mechanism that works perfectly in test and seizes in flight. See Structures and mechanisms.
References
- Flores-Abad, A. et al. “A review of space robotics technologies for on-orbit servicing”, Progress in Aerospace Sciences, 68:1, 2014.
- Maimone, M., Cheng, Y. and Matthies, L. “Two years of visual odometry on the Mars Exploration Rovers”, Journal of Field Robotics, 24:169, 2007.
- Rekleitis, I. et al. “Autonomous capture of a tumbling satellite”, Journal of Field Robotics, 24:275, 2007.
- Smith, T. et al. “Astrobee: A New Platform for Free-Flying Robotics on the International Space Station”, i-SAIRAS 2016.
- Forshaw, J. L. et al. “RemoveDEBRIS: An in-orbit active debris removal demonstration mission”, Acta Astronautica, 127:448, 2016.