Design of the Electronics Subsystem for a High-Resolution Electro-Optical Payload Using Systems Engineering Approach

dc.contributor.advisorMartinez, Peter
dc.contributor.authorMehmood, Nasir
dc.date.accessioned2023-03-31T08:19:30Z
dc.date.available2023-03-31T08:19:30Z
dc.date.issued2022
dc.date.updated2023-03-30T08:10:16Z
dc.description.abstractSatellite imagers, in contrast to commercial imagers, demand exceptional performance and operate under harsh conditions. The camera is an essential part of an Earth Observation Electro Optical (EO) payload that is designed in response to needs such as military demands, changes in world politics, inception of new technologies, operational requirements and experiments. As one of the key subsystems, the Imager Electronics Subsystem of a high-resolution EO payload plays very important role in the accomplishment of mission objectives and payload goals. Hence, these Electronics Subsystems require a special design approach optimised for their needs and meticulous characterizations of high-resolution space applications. This dissertation puts forward the argument that the system being studied is a subsystem of a larger system and that systems engineering principles can be applied to the subsystem design process also. The aim of this dissertation is to design the Imager Electronics Subsystem of a high-resolution Electro Optical Payload using a systems engineering approach to represent a logical integration and test flow using the space industry guidelines. The Imager Electronics Subsystem consists of group of elements forming the functional chain from the Image Sensors on the Focal Plane down to electrical interface to the Data Handling Unit and power interface of the satellite. This subsystem is responsible for collecting light in different spectral bands, converting this light to data of different spectral bands from image sensors for high-resolution imaging, performing operations for aligning, tagging and multiplexing along with incorporating internal and external interfaces.
dc.identifier.apacitationMehmood, N. (2022). <i>Design of the Electronics Subsystem for a High-Resolution Electro-Optical Payload Using Systems Engineering Approach</i>. (). ,Faculty of Engineering and the Built Environment ,Department of Electrical Engineering. Retrieved from http://hdl.handle.net/11427/37610en_ZA
dc.identifier.chicagocitationMehmood, Nasir. <i>"Design of the Electronics Subsystem for a High-Resolution Electro-Optical Payload Using Systems Engineering Approach."</i> ., ,Faculty of Engineering and the Built Environment ,Department of Electrical Engineering, 2022. http://hdl.handle.net/11427/37610en_ZA
dc.identifier.citationMehmood, N. 2022. Design of the Electronics Subsystem for a High-Resolution Electro-Optical Payload Using Systems Engineering Approach. . ,Faculty of Engineering and the Built Environment ,Department of Electrical Engineering. http://hdl.handle.net/11427/37610en_ZA
dc.identifier.ris TY - Master Thesis AU - Mehmood, Nasir AB - Satellite imagers, in contrast to commercial imagers, demand exceptional performance and operate under harsh conditions. The camera is an essential part of an Earth Observation Electro Optical (EO) payload that is designed in response to needs such as military demands, changes in world politics, inception of new technologies, operational requirements and experiments. As one of the key subsystems, the Imager Electronics Subsystem of a high-resolution EO payload plays very important role in the accomplishment of mission objectives and payload goals. Hence, these Electronics Subsystems require a special design approach optimised for their needs and meticulous characterizations of high-resolution space applications. This dissertation puts forward the argument that the system being studied is a subsystem of a larger system and that systems engineering principles can be applied to the subsystem design process also. The aim of this dissertation is to design the Imager Electronics Subsystem of a high-resolution Electro Optical Payload using a systems engineering approach to represent a logical integration and test flow using the space industry guidelines. The Imager Electronics Subsystem consists of group of elements forming the functional chain from the Image Sensors on the Focal Plane down to electrical interface to the Data Handling Unit and power interface of the satellite. This subsystem is responsible for collecting light in different spectral bands, converting this light to data of different spectral bands from image sensors for high-resolution imaging, performing operations for aligning, tagging and multiplexing along with incorporating internal and external interfaces. DA - 2022_ DB - OpenUCT DP - University of Cape Town KW - Space Studies LK - https://open.uct.ac.za PY - 2022 T1 - Design of the Electronics Subsystem for a High-Resolution Electro-Optical Payload Using Systems Engineering Approach TI - Design of the Electronics Subsystem for a High-Resolution Electro-Optical Payload Using Systems Engineering Approach UR - http://hdl.handle.net/11427/37610 ER - en_ZA
dc.identifier.urihttp://hdl.handle.net/11427/37610
dc.identifier.vancouvercitationMehmood N. Design of the Electronics Subsystem for a High-Resolution Electro-Optical Payload Using Systems Engineering Approach. []. ,Faculty of Engineering and the Built Environment ,Department of Electrical Engineering, 2022 [cited yyyy month dd]. Available from: http://hdl.handle.net/11427/37610en_ZA
dc.language.rfc3066eng
dc.publisher.departmentDepartment of Electrical Engineering
dc.publisher.facultyFaculty of Engineering and the Built Environment
dc.subjectSpace Studies
dc.titleDesign of the Electronics Subsystem for a High-Resolution Electro-Optical Payload Using Systems Engineering Approach
dc.typeMaster Thesis
dc.type.qualificationlevelMasters
dc.type.qualificationlevelMPhil
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