A Value Framework to Model Space Congestion in Orbit Selection

Abstract

Low Earth Orbit (LEO) is becoming more congested, which increases the risk to space missions. Decision makers will need to consider this increase in congestion as an increased risk within their mission engineering process. This thesisproposes a methodology to create and implement a value structure that quantitatively scores a range of orbits based on congestion factors of each orbit and how well each orbit meets mission requirements. This thesis demonstrates this methodology on a set of circular LEO orbits defined by altitude and inclination, and scores this illustrative scenario based on notional mission measures and expected number of encounters as congestion measures. These scores are analyzed for sensitivity to changes in orbit scoring recommendations if the decision maker were to change the importance levels between mission and congestion factors. For any given mission definition, this orbit scoring methodology can be used to identify high value orbits that would be critical to controlling space.

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Document Details

Document Type
Technical Report
Publication Date
Mar 24, 2022
Accession Number
AD1170686

Entities

People

  • Anthony J. Correale

Organizations

  • Air Force Institute of Technology

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Air Force
  • Altitude
  • Apogees
  • Artificial Satellites
  • Astronautics
  • Collision Avoidance
  • Earth Orbits
  • Elliptical Orbits
  • Engineering
  • Low Earth Orbits
  • Orbital Mechanics
  • Perigees
  • Solar Panels
  • Space Debris
  • Space Force
  • Space Missions
  • Space Objects
  • Spacecraft
  • Spacecraft Orbits
  • United States

Readers

  • Computer Networking
  • Life Cycle Cost Analysis
  • Space Exploration and Orbital Mechanics.

Technology Areas

  • Space
  • Space - Orbital Debris