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Massachusetts Institute of Technology

An integrated evolutionary model approach to small satellite engineering

Abstract

dc:description.abstract

A deficiency exists in the use of detailed integrated modeling in the design, fabrication, and operations of small satellites (<180kg). This need led to the design of the Integrated Evolutionary Model (IEM) approach to small satellite engineering. The IEM approach uses integrated modeling throughout the satellite design life cycle to support the verification and validation of the satellite capabilities and limitations. This thesis describes the IEM approach and introduces its products: a detailed command-based integrated simulation (SIM), telemetry and data analyzer (TDA), and a mission assurance tool (MAT). Recently developed integrated systems models for the MOTV and CASTOR satellites are described and critiqued against the IEM approach, and a new simulation framework is developed for CASTOR utilizing the IEM framework. The development and use of a TDA for the FalconSAT-3 satellite is also described. The thesis presents several FalconSAT-3 operational events where the TDA was paramount in identifying and characterizing unexpected on-orbit behaviors during spacecraft and experiment operations. The utility of the IEM products is demonstrated through the successful use of the FalconSAT-3 TDA in these events.

Degree

thesis:*
Department dc:contributor.department
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.
Grantor dc:publisher
Massachusetts Institute of Technology
Year dc:date.issued
2010

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Robinson, Joseph B. (Joseph Brian)
Advisor dc:contributor.advisor
  • John Keesee and Dave Miller.

Subjects

dc:subject × 1

Rights

dc:rights
Statement dc:rights
  • M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.
Language dc:language.iso
eng

Identifiers

dc:identifier.*
Handle dc:identifier.uri
http://hdl.handle.net/1721.1/59565
OAI identifier oai:identifier
oai:dspace.mit.edu:1721.1/59565

Chain of custody

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

Robinson, Joseph B. (Joseph Brian). An integrated evolutionary model approach to small satellite engineering. Massachusetts Institute of Technology, 2010. http://hdl.handle.net/1721.1/59565