Manipulators for Solar System Exploration

Manipulators for Solar System Exploration

Last Updated:December 28, 2003

In the forty years of Solar System exploration with unmanned probes, many of the missions that landed on the surface of other celestial bodies carried manipulators. Two different typologies of manipulators can be distinguished:
 

  • Single action manipulators, deployable only once and not provided with control systems on their joint.
  • Robotic Arms, with complex control and actuation controls and complex architectures.

  • To the first kind belong the arms carried on the Moon by Luna-13, on Mars by Mars-2, -3 and -6 and on Venus by Venera-13 and -14.
    Luna-13 was an E-6 type lunar lander carrying two manipulators actuated by torsion springs, each of which had six degrees of freedom. The first arm carried a small quantity of Cesium-137 to study the density of the terrain, while the second carried a wedge shaped penetrometer. Mars-2, -3 and -6 carried the PrOP-M microrover on their six degrees of freedom booms. Venera-13 and -14 carried a two degrees of freedom spring loaded manipulator carrying a penetrometer.
     

    Luna-13 showing its two spring actuated booms 

    Of course, manipulators of the second kind, with actuation and control system are much more interesting. This kind of manipulators were flown on the lunar Surveyor-3, -4 and -7 probes, on Luna-15, -16, -18 and -20, on the two Viking Mars landers and on the ill-fated Mars Polar Lander (MPL).

    The robotic arms mounted on the american Surveyor probes (known as SMSS, Soil Mechanics Surface Sampler), which landed on the moon in 1967 and 1968 were the most complex ones for what concerns the mechanical configuration. They consisted of a pantograph arm (of varying length) with three degrees of freedom: azimuth (112 degrees total angular movement), elevation (42 degrees total) and of course length (from a minimum of 58 to a maximum of 150 cm). The "end effector" of this robotic arm was a soil sampler with fixed orientation. A fourth actuator commanded the opening or closing of the sampler. This robotic arm was used to dig trenches, test the density of the soil, weight rocks, break pebbles to measure their mechanical characteristics and to move the alpha ray spectrometer from one position to another during the Surveyor-7 mission.

    Left: the Surveyor robotic arm SMMS. This is an  enlargement of the Surveyor image in the Gallery.
    Below: the kinematic configuration of the SMSS.

    The Soviet E-8-5 probes named Luna-15, -16, -18 and -20 (1969-1972) all carried on the Moon a robotic arm whose mission was to bring an hollow drill in direct contact with the soil to collect samples and then to move the samples from the sampling area to an Earth return capsule. The manipulator mounted on these missions had two degrees of freedom: elevation (100 degrees of angular excursion) and wrist rotation (180 degrees).
    The arm was carried to the Moon in a stored position alongside the body of the probe. Once on the surface, the arm was moved to a vertical configuration and the wrist was rotated 180 degrees. The drill was then lowered to the surface. The whole manoeuvre took 17.5 minutes. The wrist apparently could be used to clear the drilling area of small rocks by moving it some degree clockwise and anticlockwise of the reference position. Because of the simplicity of the arm, the system could only collect samples from a well defined position with respect to the probe. The sample unloading sequence was the exact reverse of the arm deploying one. Luna-15 and -18 failed, while Luna-16 returned 101 g of lunar soil to Earth and Luna-20 some 30 g from the lunar highlands. The later Luna-23 and -24 missions carried a completely redesigned sample collecting system using a rail mounted 2 meters long drill instead of the robotic arm.
     
    Above: the E-8-5 ascent stage and instrument module showing the robotic arm on the right.
    Below: The deploying sequence of the E-8-5 robotic arm from the stowed position to the sample drilling position

    The two Viking probes, which landed on Mars in 1976 all carried a robotic arm to collect samples from the terrain and to hand them to various scientific instruments. The manipulator had four degrees of freedom: azimuth (120 degrees of angular excursion), elevation, wrist rotation and length. The arm was made of telescoping sections, enabling it to vary its length to a maximum of three meters. The end effector was a small sampler using some simple instruments to measure the mechanical characteristics of the soil and to verify the presence of iron using small magnets.
    The manipulator was extended to collect samples and then retracted and positioned over one of the many scientific instruments of the probe. Sample unloading was accomplished by rotating the sampler wrist by 180 degrees. The Viking robot arm was a critical component for the mission since it was to hand over samples to the most important scientific instruments for analysis (five instruments, including the three dedicated to organic life detection).
    Left: The Viking robot arm in action (NASA Image).
    Below: The kinematic configuration of the robot arm.

    The Mars Polar Lander (MPL) probe, lost while landing in december 1999 carried the most complex robotic manipulator ever flown on a planetary mission. The main characteristics of this robotic arm were:
     

  • Four degrees of freedom: three in elevation, one in azimuth
  • Low weight (3.5 kg mass for a 2.2 meters length) construction in graphite and epoxy resin
  • Minimal power requirements: the nominal budget being 10 W and the maximum allowed 20W
  • Ample choice of end effectors: a sample collector, a rake, a temperature sensor mounted on a 15 cm spike that could be inserted into the soil and a small camera, mounted before the fourth joint and used to monitor the digging operations and to perform a visual inspection of the samples.

  • Many samples collected by the manipulator were then handed to an instrument designed to find traces of water.
    The manipulator manoeuvres were extremely slow (tenths of degrees per second) to minimize the size of the actuators and the energy requirements. Depending on the posture, the arm was able to reach a cartesian end effector speed of up to 7 cm/s and to exercise a 80 N force.
    Beside an "operational" role, the MPL robotic arm was conceived as a real scientific instrument, for it could be used to perform mechanical soil characterization.
    A very similar manipulator to this one was to have been carried on the canceled Mars Surveyor 2001 Lander.
    In this case, the possible end effector included a sample collector, a rake, an electrometer to measure triboelectric charges caused by the rubbing of the collector against the Martian surface and to measure ionization of the atmosphere and an hook to move a small rover similar to Sojourner from its flight position on top of the lander to the surface. The rover deploying manoeuvre was considered very critical and was to have been preceded by a 3D photographic survey of the terrain on which the rover would "land". The manoeuvre was to have been accomplished by lowering the rover 3 cm at a time until the manipulator would have signaled its "unloaded" status.
    Left: The Mars Polar Lander robotic arm completely deployed (NASA Image)
    Right: The kinematic configuration of the MPL robotic arm

    Another manipulator is mounted the Beagle 2 European Mars Lander. The robotic arm weighs 2.64 kg and is designed to bring many scientific instruments in contact with the ground, including the sample collecting "mole"


    An image of the British Beagle II Mars lander showing the robotic arm.
    Image Copyright Paolo Ulivi

    And recently, China has announced to be studying a robotic manipulator for collecting samples on the Moon. The analysis of this statement is on my Chinese planetary program page.

    Finally, a very complex manipulator was to have flown on NASA's Mars Sample Return mission in 2003.
    This was to have been built in Italy and was a four degree of freedom manipulator, just like the Mars Polar Lander One. As an end effector, however, the manipulator was to have carried a drill box, inside which there was a 50 cm long drill and sample retriever, the drill rotation and translation electric motors, some scientific instrument and a carousel cache for sample storage. The arm was abel to hand its samples to either the MAV (Mars Ascent Vehicle) rocket for Earth return or to scientific instruments part of the ASE (Additional Science Envelope) and IPSE (Italian Package for Science Experiment) packages. The total weight of the manipulator was approximately 15 kg, most of which was made up by the drill box. Unfortunately, the mission was canceled after the loss of Mars Polar Lander.

    The MSR probe, showing the four degrees of freedom robotic manipulator and drill box in dark brown.

    BIBLIOGRAPHY
    Beagle 2: Robotic Arm
    Bonitz, R.G., Nguyen, T.T., Kim, W.S.: The Mars Surveyor '01 Rover and Robotic Arm
    Bonitz, R.G.: Mars Surveyor '98 Lander MVACS Robotic Arm Control System Design Concepts, Proceedings of the IEEE International Conference on Robotics and Automation, 1997, pp. 2465-2470
    Bonitz, R.G:: MVACS Robotic Arm. Available on line
    Ezell, E. C., Ezell. L. N. "On Mars", NASA SP-4212, Available on-line
    Wilson, A.: Solar System Log, Jane's, London
    Ulivi, P.: Studio di Ottimizzazione ad Energia Minima per un Manipolatore per l'Esplorazione di Marte. Master Thesis, Politecnico di Milano, 2000

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