Please use this identifier to cite or link to this item: http://10.1.7.192:80/jspui/handle/123456789/12348
Full metadata record
DC FieldValueLanguage
dc.contributor.authorPrajapati, Vijay-
dc.date.accessioned2024-07-29T04:57:21Z-
dc.date.available2024-07-29T04:57:21Z-
dc.date.issued2024-06-01-
dc.identifier.urihttp://10.1.7.192:80/jspui/handle/123456789/12348-
dc.description.abstractAn accurate positioning system is required to precisely adjust the mirrors of a space telescope, and efforts have been made for developing such a system. This telescope is intended to be accommodated within launch vehicles and incorporates segmented mirrors to effectively accommodate large mirrors. Following the unfolding process, the segmented primary mirror becomes pivotal in focusing light from distant celestial bodies. The configuration of these segmented mirrors significantly influences the resulting image quality. To address this, six actuators have been designated for the six degrees of freedom of these segmented mirrors. They are strategically positioned behind each segment, allowing for both fine-tuning and coarse adjustment. As the full mirror is divided into smaller segments, meticulous design is essential to ensure seamless alignment after unfolding and positioning. These actuators are constructed using commonly available mechanical components, such as flexures, gears, bearings, camshafts, and ball screws. The coarse-drive Tumbler coupling facilitates independent fine motion control. The engagement of these shafts produces combined motion, while disengagement results in only fine motion. A crucial component of the design is the motion reduction structure, a sophisticated passive system that smoothly converts coarse input (in micrometers) into precise output (in nanometers) without any backlash. The actuators have been assembled and tested which deliver both coarse and fine motion adjustments, achieving a remarkable resolution of less than 10 nanometers across a 5-millimeter range. A comprehensive control mechanism, inclusive of feedback control, is implemented to precisely manage both coarse and fine motions, achieving the desired positions. In the initial phase, two actuators are integrated into bipod structures for 2 degrees of freedom control. Subsequently, the study progresses to the hexapod assembly and control and optimization techniques involved in developing the actuators and the entire 6 degrees of freedom hexapod assembly.en_US
dc.publisherInstitute of Technologyen_US
dc.relation.ispartofseries22MMCC12;-
dc.subjectMechanical 2022en_US
dc.subjectProject Reporten_US
dc.subjectProject Report 2022en_US
dc.subjectMechanical Project Reporten_US
dc.subject22MMCen_US
dc.subject22MMCCen_US
dc.subject22MMCC12en_US
dc.subjectCAD/CAMen_US
dc.subjectCAD/CAM 2022en_US
dc.subjectActuatorsen_US
dc.subjectTelescopeen_US
dc.subjectMonolithic mirroren_US
dc.subjectegmented Mirror and Segmented Mirror Telescopeen_US
dc.subjectBipod Arrangementen_US
dc.subjectHexapod Systemen_US
dc.titleDesign, Development and Ground Testing of the Hexapod Systemen_US
dc.typeDissertationen_US
Appears in Collections:Dissertation, ME (CAD/CAM)

Files in This Item:
File Description SizeFormat 
22MMCC12.pdf22MMCC123.79 MBAdobe PDFView/Open


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.