{"id":{"repo_id":"uiuc","oai_identifier":"oai:www.ideals.illinois.edu:2142/125623"},"canonical_url":"https://search.dev.ndltd.org/etd/uiuc/oai:www.ideals.illinois.edu:2142/125623","repository":{"repo_id":"uiuc","name":"University of Illinois - Urbana-Champaign","base_url":"https://www.ideals.illinois.edu/oai-pmh"},"display":{"title":"Implementation of a configurable small satellite design and mission planning tool","abstract":"Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2025-02-04 without embargo terms","abstract_html":"Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2025-02-04 without embargo terms","abstract_has_math":false,"creators":["Harrigan, Michael"],"institution":"University of Illinois at Urbana-Champaign","degree_name":"M.S.","degree_level":"Thesis","degree_discipline":"Aerospace Engineering","degree_department":null,"school":null,"contributors":["Lembeck, Michael F"],"advisors":[],"committee_chairs":[],"committee_members":[],"year":2024,"date_issued":"2024-07-17","date_published":"2024-07-17","updated_at":"2026-07-22T22:25:02Z","subjects":["Freeflyer","Aerospace Systems Engineering","Design Optimization","Satellite","Small Satellite","Cubesat","Mission Planning","Power System Sizing","Link Budget","Power Budget","Force Modeling","Data Budget","Lassi","Mission Design","Orbital Simulation"],"languages":["en","eng"],"rights":["© 2024 Michael Harrigan"],"rights_urls":[],"identifier_entries":[]},"links":{"outbound_url":"https://hdl.handle.net/2142/125623","outbound_label":"Handle","outbound_source":"dc:identifier"},"metadata_groups":[{"id":"people","label":"People","entries":[{"key":"dc:contributor","label":"Contributor","values":["Lembeck, Michael F"]},{"key":"dc:creator","label":"Author","values":["Harrigan, Michael"]}]},{"id":"academic_context","label":"Academic Context","entries":[{"key":"dc:date","label":"Dc Date","values":["2024-07-17","2024-08"]},{"key":"dc:type","label":"Dc Type","values":["text","Thesis"]},{"key":"thesis:degree_discipline","label":"Discipline","values":["Aerospace Engineering"]},{"key":"thesis:degree_level","label":"Degree Level","values":["Thesis"]},{"key":"thesis:degree_name","label":"Degree Name","values":["M.S."]},{"key":"thesis:institution_name","label":"Thesis Institution Name","values":["University of Illinois at Urbana-Champaign"]}]},{"id":"subjects_keywords","label":"Subjects and Keywords","entries":[{"key":"dc:subject","label":"Dc Subject","values":["Freeflyer","Aerospace Systems Engineering","Design Optimization","Satellite","Small Satellite","Cubesat","Mission Planning","Power System Sizing","Link Budget","Power Budget","Force Modeling","Data Budget","Lassi","Mission Design","Orbital Simulation"]}]},{"id":"language_rights","label":"Language and Rights","entries":[{"key":"dc:language","label":"Dc Language","values":["en","eng"]},{"key":"dc:rights","label":"Dc Rights","values":["© 2024 Michael Harrigan"]}]},{"id":"identifiers","label":"Identifiers","entries":[{"key":"dc:identifier","label":"Identifier","values":["https://hdl.handle.net/2142/125623"]}]},{"id":"additional","label":"Additional Metadata","entries":[{"key":"dc:description","label":"Description","values":["Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2025-02-04 without embargo terms","The student, Michael Harrigan, accepted the attached license on 2024-07-12 at 01:14.","The student, Michael Harrigan, submitted this Thesis for approval on 2024-07-12 at 01:27.","This Thesis was approved for publication on 2024-07-17 at 11:08.","DSpace SAF Submission Ingestion Package generated from Vireo submission #21085 on 2025-02-04 at 21:05:11","This thesis introduces an implementation of a configurable small satellite mission design tool based on a. i. Solutions’ FreeFlyer™ platform. Designing and operating small satellite missions poses significant challenges due to their size and mass constraints. Small satellites have limited resources and constrained capabilities, such as attitude control, power, and communication. Optimizing the performance of these subsystems is crucial for ensuring mission success and maximizing scientific return. To address these challenges, a comprehensive, integrated tool for small satellite mission design and analysis is needed. FreeFlyer™ provides a highly customizable, robust, and reliable framework for orbital performance simulations. A vital feature of the tool is its ability to script adaptive mission plans. The tool supports a wide range of orbit types, propagators, maneuvers, models, and output options for modeling and simulating complex space scenarios. The tool allows users to define and adjust satellite system parameters (e.g., satellite pointing configurations, attitude control devices, solar array and battery sizing, and communications link budgets) in a unified analysis and simulation environment to evaluate the possible trade-offs in performance against resource costs for various design choices. A survey of existing programs and their shortcomings is explored. A description of an improved tool is provided, and examples of its applications demonstrate its effectiveness in optimizing and validating a previously designed small satellite mission. These case studies illustrate the tool’s usefulness in sizing critical mission components and showcase its potential to expedite the small satellite mission design process."]},{"key":"dc:format","label":"Dc Format","values":["application/pdf"]},{"key":"dc:title","label":"Title","values":["Implementation of a configurable small satellite design and mission planning tool"]}]}],"canonical_facts":{"dc:contributor":["Lembeck, Michael F"],"dc:creator":["Harrigan, Michael"],"dc:date":["2024-07-17","2024-08"],"dc:description":["Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2025-02-04 without embargo terms","The student, Michael Harrigan, accepted the attached license on 2024-07-12 at 01:14.","The student, Michael Harrigan, submitted this Thesis for approval on 2024-07-12 at 01:27.","This Thesis was approved for publication on 2024-07-17 at 11:08.","DSpace SAF Submission Ingestion Package generated from Vireo submission #21085 on 2025-02-04 at 21:05:11","This thesis introduces an implementation of a configurable small satellite mission design tool based on a. i. Solutions’ FreeFlyer™ platform. Designing and operating small satellite missions poses significant challenges due to their size and mass constraints. Small satellites have limited resources and constrained capabilities, such as attitude control, power, and communication. Optimizing the performance of these subsystems is crucial for ensuring mission success and maximizing scientific return. To address these challenges, a comprehensive, integrated tool for small satellite mission design and analysis is needed. FreeFlyer™ provides a highly customizable, robust, and reliable framework for orbital performance simulations. A vital feature of the tool is its ability to script adaptive mission plans. The tool supports a wide range of orbit types, propagators, maneuvers, models, and output options for modeling and simulating complex space scenarios. The tool allows users to define and adjust satellite system parameters (e.g., satellite pointing configurations, attitude control devices, solar array and battery sizing, and communications link budgets) in a unified analysis and simulation environment to evaluate the possible trade-offs in performance against resource costs for various design choices. A survey of existing programs and their shortcomings is explored. A description of an improved tool is provided, and examples of its applications demonstrate its effectiveness in optimizing and validating a previously designed small satellite mission. These case studies illustrate the tool’s usefulness in sizing critical mission components and showcase its potential to expedite the small satellite mission design process."],"dc:format":["application/pdf"],"dc:identifier":["https://hdl.handle.net/2142/125623"],"dc:language":["en","eng"],"dc:rights":["© 2024 Michael Harrigan"],"dc:subject":["Freeflyer","Aerospace Systems Engineering","Design Optimization","Satellite","Small Satellite","Cubesat","Mission Planning","Power System Sizing","Link Budget","Power Budget","Force Modeling","Data Budget","Lassi","Mission Design","Orbital Simulation"],"dc:title":["Implementation of a configurable small satellite design and mission planning tool"],"dc:type":["text","Thesis"],"thesis:degree_discipline":["Aerospace Engineering"],"thesis:degree_level":["Thesis"],"thesis:degree_name":["M.S."],"thesis:institution_name":["University of Illinois at Urbana-Champaign"]},"updated_at":"2026-07-22T22:25:02Z"}