Building on the success of the two rover geologists that arrived to Mars in January, 2004, NASA's next rover mission is
planned for the end of the decade. Twice as long and three times as heavy as Spirit and Opportunity, the Mars Science
Laboratory rover will collect Martian soil samples and rock cores and analyze them for organic compounds and
environmental conditions that could have supported microbial life now or in the past. MSL meteorological package is
called REMS (Rover environmental Monitoring Station). This is a scientific instrument designed to provide in situ,
near-surface measurements of Temperature (ground surface and atmosphere), Wind, Pressure, Water Vapour and
Ultraviolet Radiation (UV). UV observations at the surface will provide important information necessary to asses the
habitability of the near surface environment.
REMS UV sensor on MSL rover shall be pointing to the Martian sky. From the beginning, deposition of dust particles
on the sensor head was considered by NASA's science office a major concern. Such unpredictable phenomena may
attenuate the signal received by the optical sensor, and therefore must be considered by far the largest source of error in
the sensor.
We have studied the error introduced by Martian dust deposition, as well as by frost formation on REMS UV sensor.
Several error mitigation strategies such as the use of magnets where evaluated. Finally, a robotic dust wiper was
selected as error mitigation system. An optical sensor with a dust wiper was designed, constructed and pre-qualified for
MSL mission.
Several brushes where fabricated and tested as to maximize its efficiency with submicron particles dust. An
Engineering Model of the Sensor including the dust Wiper technology was fabricated and tested. The prototype was
subjected to an early qualification campaign under MSL project requirements. Technology performance and
qualification results are presented in this paper. The proposed Dust Wiper technology proves to be a simple, yet
effective solution to mitigate the error caused by dust on optical sensors or solar panels operating on dirty atmospheres.
Using a novel actuator technology based on SMA fibers, the solution represents a very small increase in Mass and a
major improvement in system performance. The actuator technology is now being considered for industrial sectors
where mass, reliability and cost reduction are key design goals.
In response to a clear need, the research community on EAP (Electroactive Polymer) has just started to work on a standard test methodology to characterize EAP actuators. A very general test methodology for EAPs, covering the characterization procedures for extensional and bending actuators was recently presented. In the present work, well known IPMC samples are characterized following such test methodology. Also, additional tests, not covered by the preliminary standard are included. These tests are conducted using the EAP Unit Tester, a test bench specifically designed for the characterization of EAP actuators. Rather than presenting new material's results, the paper focuses on the instrumentation, procedures and form of presenting results. Although the paper is focused on IPMC the method can be extrapolated to other bending actuators.
In order to make EAP actuators technology scalable a design methodology for polymer actuators is required. Design variables, optimization formulas and a general architecture are required as it is usual in electromagnetic or hydraulic actuators design. This will allow the development of large EAP actuators from micro-actuator units, specifically designed for a particular application. It will also help to enhance the EAP material final performance. This approach is not new, since it is found in Nature. Skeletal muscle architecture has a profound influence on muscle force-generating properties and functionality. Based on existing literature on skeletal muscle biomechanics, the Nature design philosophy is inferred. Formulas and curves employed by Nature in the design of muscles are presented. Design units such as fiber, tendon, aponeurosis, and motor units are compared with the equivalent design units to be taken into account in the design of EAP actuators. Finally a complete design methodology for the design of actuators based on multiple EAP fiber/sheets is proposed. In addition, the procedure gives an idea of the required parameters that must be clearly modeled and characterized at EAP material level prior to attempt the design of complex Electromechanical Systems based on Electroactive Polymers.
Current EAP actuator sheets or fibers perform reasonable well in the centimeter and mN range, but are not practical for larger force and deformation requirements. In order to make EAP actuators technology scalable a design methodology for polymer actuators is required. Design variables, optimization formulas and a general architecture are required, as it is usual in electromagnetic or hydraulic actuator design. This will allow the development of large EAP actuators specifically designed for a particular application. It will also help to enhance the EAP material final performance. This approach is not new, it is found in Nature. Skeletal muscle architecture has a profound influence on muscle force-generating properties and functionality. Based on existing literature on skeletal muscle biomechanics, the Nature design philosophy is inferred. Formulas and curves employed by Nature in the design of muscles are presented. Design units such as fiber, tendon, aponeurosis, and motor unit are compared with the equivalent design units to be taken into account in the design of EAP actuators. Finally a complete design methodology for the design of actuators based on multiple EAP fiber is proposed. In addition, the procedure gives an idea of the required parameters that must be clearly modeled and characterized at EAP material level.
Since the field of Electroactive Polymers (EAP) actuators is fairly new there are no standard testing processes for such intelligent materials. This drawback can seriously limit the scope of application of EAP actuators, since the targeted industrial sectors (aerospace, biomedical...) demand high reliability and product assurance. As a first iteration two elements are required to define a test standard for an EAP actuator: a Unit Tester, and a Component Specification. In this paper a EAP Unit Tester architecture is presented along with the required classification of measurements to be included in the EAP actuator Component Specification. The proposed EAP Unit Tester allows on-line monitoring and recording of the following properties of the specimen under test: large deformation, small tip displacement, temperature at the electrodes, weight of the specimen, voltage and current driven into the EAP, load being applied to the actuator, output voltage of the EAP in sensing operation and mode of operation (structure/sensor/actuator/smart). The measurements are taken simultaneously, in real-time. The EAP Unit Tester includes a friendly Graphical User Interface. It uses embedded Excel tools to visualize data. In addition, real-time connectivity with MATLAB allows an easy testing of control algorithms. A novel methodology to measure the properties of EAP specimens versus a variable load is also presented. To this purpose a force signals generator in the range of mN was developed. The device is based on a DC mini-motor. It generates an opposing force to the movement of the EAP actuator. Since the device constantly opposes the EAP actuator movement it has been named Digital Force Generator (DFG). The DFG design allows simultaneous length and velocity measuring versus different load signals. By including such a device in the EAP Unit Tester the most suitable application for the specimen under test can be easily identified (vibration damper, large deformation actuator, large force actuator, fast actuator...).
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