Synthesis of Tolerances for Spacecraft Mechanism |
Author(s): |
| Sulficker Ali Ismail , P. G. Scholar, Department of Mechanical Engineering, Mar Athanasius College of Engineering, Kothamangalam, Kerala, India; N. Sujithkumar, Scientist/Engineer, Reliability Assurance Mechanical Division, Systems Reliability Group, ISRO Satellite Centre, Bangalore, Karnataka, India; J. Dileeplal, Associate Professor, Department of Mechanical Engineering, Mar Athanasius College of Engineering, Kothamangalam, Kerala, India; Y. S. Shankar Narayan, Scientist/Engineer, Reliability Assurance Mechanical Division, Systems Reliability Group, ISRO Satellite Centre, Bangalore, Karnataka, India |
Keywords: |
| Tolerance Analysis, root sum square method, Assembly Simulation by Software R |
Abstract |
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Tolerance have a great impact on the quality and cost of the mechanism. Proper tolerance design enables complex mechanical assemblies consisting of numerous parts to assemble and work together in a proper manner so that they fulfill their design objectives. In this paper the tolerance of a spacecraft mechanism is analyzed using worst case and root sum square method. The tolerance synthesis of the spacecraft mechanism is done by direct linearization method. |
Other Details |
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Paper ID: IJSRDV3I100292 Published in: Volume : 3, Issue : 10 Publication Date: 01/01/2016 Page(s): 385-387 |
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