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Massachusetts Institute of Technology

Development of a Special Purpose End-to-End Satellite Constellation Design Methodology

Abstract

dc:description.abstract

Recent improvements in payload delivery to low-Earth orbit (LEO) have significantly improved the capacity to economically deploy satellite constellations. These constellations are profoundly versatile, with the potential to allow researchers to gather large volumes of data from astronomy and Earth-observing missions over an unconstrained mission lifetime. However, many current satellite constellation design methodologies focus on designing satellite constellations with global coverage, rather than constellations with maximized coverage for a smaller, specified area of interest. This dissertation presents an open-source methodological framework capable of optimizing the design of special purpose satellite constellations for a given mission science objective. We present two case studies that we use to illustrate the framework’s functionality. The first case study is an astronomy constellation, with a science objective that maximizes coverage of a list of target stars so that we can minimize the error of stellar spin-axis inclination retrieval and constrain the spin-axis inclination of FGK spectral-type target stars. The second case study is an Earth-observing constellation designed to minimize revisit time to a specific target area, and achieve better ground sampling precision over existing thermal infrared platforms for the monitoring of thermal emissions over a target area. Our special purpose framework is robust, modular, and fast, allowing it to serve as an effective reference point for any commercial, scientific, and governmental mission requiring satellite constellation design. We find Pareto optimal satellite constellation architectures for a thermal infrared Earth-observing mission that achieve a minimum revisit time of 8 days for a ground sampling distance of 6.6 m.

Degree

thesis:*
Name thesis:degree_name
Doctoral
Department dc:contributor.department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Grantor dc:publisher
Massachusetts Institute of Technology
Year dc:date.issued
2023

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Cummings, Andrew T.
Advisors dc:contributor.advisor
  • Seager, Sara
  • de Weck, Olivier
  • Linares, Richard

Rights

dc:rights
Statement dc:rights
  • In Copyright - Educational Use Permitted
  • Copyright MIT

Identifiers

dc:identifier.*
Handle dc:identifier.uri
https://hdl.handle.net/1721.1/154189
OAI identifier oai:identifier
oai:dspace.mit.edu:1721.1/154189

Chain of custody

source
Harvested from
MIT
Base URL
dspace.mit.edu/oai/request
Last updated
2026-07-22
Source record
OAI-PMH GetRecord
related terms
citation

Cummings, Andrew T.. Development of a Special Purpose End-to-End Satellite Constellation Design Methodology. Massachusetts Institute of Technology, 2023. https://hdl.handle.net/1721.1/154189