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The focal plane unit plays a vital role in an earth observation payload to meet its highly demanding optical performance requirements. Focal plane unit mechanics consist of a sensor module mounting and planar optics. An image is formed on the image plane and mechanics is used to hold sensors and pla...
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| Format: | Thesis |
| Language: | English |
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Department of Electrical Engineering
2023
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| _version_ | 1867613331680919552 |
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| access_status_str | Open Access |
| author | Anwar, Muhammad Mubeen |
| author2 | Martinez, Peter |
| author_browse | Anwar, Muhammad Mubeen Martinez, Peter |
| author_facet | Martinez, Peter Anwar, Muhammad Mubeen |
| author_sort | Anwar, Muhammad Mubeen |
| collection | Thesis |
| description | The focal plane unit plays a vital role in an earth observation payload to meet its highly demanding optical performance requirements. Focal plane unit mechanics consist of a sensor module mounting and planar optics. An image is formed on the image plane and mechanics is used to hold sensors and planar optics in place. The mechanical design of this unit is has two functions. Firstly, it ensures optical focus and alignment of the image plane in the temperature extremes of the space environment. Secondly, the mechanics also needs to handle harsh launching loads to get the satellite in space. The important constraints of this design are the mass and volume which need to be considered during the design. Optical performance depends a lot on the design of the mechanics used to support and align optical elements and image sensors. In this dissertation we perform the design of a focal plane unit using Solid Works 3D CAD modelling software. To validate the mechanical performance of our design Finite Element Analysis (FEM) analysis needs to be performed on every mechanical element with application of launch and environmental loads. Assembly and integration of the focal plane unit is also an important consideration, which if not properly done may deteriorate the performance. Therefore, the assembly and integration procedure is also highlighted in this work. These processes are presented in this work with future recommendations for future work. |
| format | Thesis |
| id | oai:open.uct.ac.za:11427/36990 |
| institution | University of Cape Town (South Africa) |
| language | eng |
| last_indexed | 2026-06-10T12:34:27.383Z |
| license_str | Not specified — see source repository |
| provenance_str_mv | Harvested via OAI-PMH from UCTD — University of Cape Town Open Access Repository |
| publishDate | 2023 |
| publishDateRange | 2023 |
| publishDateSort | 2023 |
| publisher | Department of Electrical Engineering |
| publisherStr | Department of Electrical Engineering |
| record_format | dspace |
| source_str | UCTD — University of Cape Town Open Access Repository |
| spelling | oai:open.uct.ac.za:11427/36990 Mechanical Structure Design and Analysis of Focal Plane Unit (Fpu) for Earth Observation (Eo) Payload Anwar, Muhammad Mubeen Martinez, Peter Space Studies The focal plane unit plays a vital role in an earth observation payload to meet its highly demanding optical performance requirements. Focal plane unit mechanics consist of a sensor module mounting and planar optics. An image is formed on the image plane and mechanics is used to hold sensors and planar optics in place. The mechanical design of this unit is has two functions. Firstly, it ensures optical focus and alignment of the image plane in the temperature extremes of the space environment. Secondly, the mechanics also needs to handle harsh launching loads to get the satellite in space. The important constraints of this design are the mass and volume which need to be considered during the design. Optical performance depends a lot on the design of the mechanics used to support and align optical elements and image sensors. In this dissertation we perform the design of a focal plane unit using Solid Works 3D CAD modelling software. To validate the mechanical performance of our design Finite Element Analysis (FEM) analysis needs to be performed on every mechanical element with application of launch and environmental loads. Assembly and integration of the focal plane unit is also an important consideration, which if not properly done may deteriorate the performance. Therefore, the assembly and integration procedure is also highlighted in this work. These processes are presented in this work with future recommendations for future work. 2023-02-23T00:37:39Z 2023-02-23T00:37:39Z 2022 2023-02-20T12:12:33Z Master Thesis Masters MPhil http://hdl.handle.net/11427/36990 eng application/pdf Department of Electrical Engineering Faculty of Engineering and the Built Environment |
| spellingShingle | Space Studies Anwar, Muhammad Mubeen Mechanical Structure Design and Analysis of Focal Plane Unit (Fpu) for Earth Observation (Eo) Payload |
| thesis_degree_str | Master's |
| title | Mechanical Structure Design and Analysis of Focal Plane Unit (Fpu) for Earth Observation (Eo) Payload |
| title_full | Mechanical Structure Design and Analysis of Focal Plane Unit (Fpu) for Earth Observation (Eo) Payload |
| title_fullStr | Mechanical Structure Design and Analysis of Focal Plane Unit (Fpu) for Earth Observation (Eo) Payload |
| title_full_unstemmed | Mechanical Structure Design and Analysis of Focal Plane Unit (Fpu) for Earth Observation (Eo) Payload |
| title_short | Mechanical Structure Design and Analysis of Focal Plane Unit (Fpu) for Earth Observation (Eo) Payload |
| title_sort | mechanical structure design and analysis of focal plane unit fpu for earth observation eo payload |
| topic | Space Studies |
| url | http://hdl.handle.net/11427/36990 |
| work_keys_str_mv | AT anwarmuhammadmubeen mechanicalstructuredesignandanalysisoffocalplaneunitfpuforearthobservationeopayload |