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  • Spacecraft Design, Testing and Performance; Structural Mechanics; Cybernetics, Artificial Intelligence and Robotics  (1)
  • Structural Mechanics; Mechanical Engineering; Aircraft Design, Testing and Performance  (1)
  • Structural Mechanics; Statistics and Probability; Man/System Technology and Life Support  (1)
  • 1
    Publication Date: 2019-07-13
    Description: This paper evaluates the development of automated assembly techniques for discrete lattice structures using a multi-axis gantry type CNC machine. These lattices are made of discrete components called "digital materials." We present the development of a specialized end effector that works in conjunction with the CNC machine to assemble these lattices. With this configuration we are able to place voxels at a rate of 1.5 per minute. The scalability of digital material structures due to the incremental modular assembly is one of its key traits and an important metric of interest. We investigate the build times of a 5x5 beam structure on the scale of 1 meter (325 parts), 10 meters (3,250 parts), and 30 meters (9,750 parts). Utilizing the current configuration with a single end effector, performing serial assembly with a globally fixed feed station at the edge of the build volume, the build time increases according to a scaling law of n4, where n is the build scale. Build times can be reduced significantly by integrating feed systems into the gantry itself, resulting in a scaling law of n3. A completely serial assembly process will encounter time limitations as build scale increases. Automated assembly for digital materials can assemble high performance structures from discrete parts, and techniques such as built in feed systems, parallelization, and optimization of the fastening process will yield much higher throughput.
    Keywords: Structural Mechanics; Mechanical Engineering; Aircraft Design, Testing and Performance
    Type: ARC-E-DAA-TN39672 , IEEE Aerospace Conference 2017; Mar 04, 2017 - Mar 11, 2017; Big Sky, MT; United States
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  • 2
    Publication Date: 2019-07-13
    Description: We describe a robotic platform for traversing and manipulating a modular 3D lattice structure. The robot is designed to operate within a specifically structured environment, which enables low numbers of degrees of freedom (DOF) compared to robots performing comparable tasks in an unstructured environment. This allows for simple controls, as well as low mass and cost. This approach, designing the robot relative to the local environment in which it operates, results in a type of robot we call a "relative robot." We describe a bipedal robot that can locomote across a periodic lattice structure, as well as being able to handle, manipulate, and transport building block parts that compose the lattice structure. Based on a general inchworm design, the robot has added functionality for traveling over and operating on a host structure.
    Keywords: Spacecraft Design, Testing and Performance; Structural Mechanics; Cybernetics, Artificial Intelligence and Robotics
    Type: ARC-E-DAA-TN38470 , AIAA SciTech 2017; Jan 09, 2017 - Jan 13, 2017; Grapevine, TX; United States
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  • 3
    Publication Date: 2019-07-13
    Description: It is widely assumed that human exploration beyond Earth's orbit will require vehicles capable of providing long duration habitats that simulate an Earth-like environment - consistent artificial gravity, breathable atmosphere, and sufficient living space- while requiring the minimum possible launch mass. This paper examines how the qualities of digital cellular solids - high-performance, repairability, reconfigurability, tunable mechanical response - allow the accomplishment of long-duration habitat objectives at a fraction of the mass required for traditional structural technologies. To illustrate the impact digital cellular solids could make as a replacement to conventional habitat subsystems, we compare recent proposed deep space habitat structural systems with a digital cellular solids pressure vessel design that consists of a carbon fiber reinforced polymer (CFRP) digital cellular solid cylindrical framework that is lined with an ultra-high molecular weight polyethylene (UHMWPE) skin. We use the analytical treatment of a linear specific modulus scaling cellular solid to find the minimum mass pressure vessel for a structure and find that, for equivalent habitable volume and appropriate safety factors, the use of digital cellular solids provides clear methods for producing structures that are not only repairable and reconfigurable, but also higher performance than their conventionally manufactured counterparts.
    Keywords: Structural Mechanics; Statistics and Probability; Man/System Technology and Life Support
    Type: ARC-E-DAA-TN39675 , IEEE Aerospace Conference 2017; Mar 04, 2017 - Mar 11, 2017; Big Sky, MT; United States
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