2014 IEEE International Conference on Technologies for Practical Robot Applications (TePRA) 2014
DOI: 10.1109/tepra.2014.6869150
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Truss assembly and welding by Intelligent Precision Jigging Robots

Abstract: This paper describes an Intelligent Precision Jigging Robot (IPJR) prototype that enables the precise alignment and welding of titanium space telescope optical benches. The IPJR, equipped with µm accuracy sensors and actuators, worked in tandem with a lower precision remote controlled manipulator. The combined system assembled and welded a 2 m truss from stock titanium components. The calibration of the IPJR, and the difference between the predicted and the truss dimensions as-built, identified additional sour… Show more

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Cited by 9 publications
(14 citation statements)
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References 8 publications
(9 reference statements)
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“…A dedicated on-orbit experiment to assemble a space telescope optical bench will require hardware that is even more precise than the sensors and actuators that we used in Komendera et al (2014a). It will also make use of external measurement systems, such as precise cameras, to further improve the estimates.…”
Section: Resultsmentioning
confidence: 99%
See 3 more Smart Citations
“…A dedicated on-orbit experiment to assemble a space telescope optical bench will require hardware that is even more precise than the sensors and actuators that we used in Komendera et al (2014a). It will also make use of external measurement systems, such as precise cameras, to further improve the estimates.…”
Section: Resultsmentioning
confidence: 99%
“…However, to be conservative in how we interpreted the precisions of the actuator and the laser sensor, and to allow room for the aforementioned physical processes, we inflated the noises to s L = 8 mm and s M = 1 mm, and simulated MLE assembly trials on the sequence in Figure 7. It is obvious that each individual strut length can only be within 16 mm 95% of the time, meaning that the tolerance of 10 mm cannot be guaranteed with the hardware we used in Komendera et al (2014a). That said, with MLE in the assembly process, the average trace is 3.13 × 10 210 m 2 , making the mean error 17.7 mm as shown in Figure 11, only slightly worse than the 16 mm per strut error.…”
Section: Discussionmentioning
confidence: 97%
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“…When this method is applied to in-space assembly, these robots are usually called "satellite arms". [11], [12], [18] With this method, the separation of the assembler from the structure requires a global external positioning system in order to align the elements, adding to the complexity and limiting the scale of the final design to that of the positioning system [11], [12], [13].…”
Section: B Robotic Assemblymentioning
confidence: 99%