53rd AIAA Aerospace Sciences Meeting 2015
DOI: 10.2514/6.2015-1623
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A Review of Impending Small Satellite Formation Flying Missions

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Cited by 70 publications
(36 citation statements)
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“…This will require some level of propulsion. Formation flying of cubesats is an active area of research, with many missions proposed as demonstrations [4]. These missions demonstrate a TRL level for formation flying and propulsion technologies at TRL6 for the concept, but more likely TRL3 for the exact requirements of the proposed mission concept.…”
Section: Propulsion and Formation Flyingmentioning
confidence: 99%
“…This will require some level of propulsion. Formation flying of cubesats is an active area of research, with many missions proposed as demonstrations [4]. These missions demonstrate a TRL level for formation flying and propulsion technologies at TRL6 for the concept, but more likely TRL3 for the exact requirements of the proposed mission concept.…”
Section: Propulsion and Formation Flyingmentioning
confidence: 99%
“…As a result, more and more space missions are designed as DSS [6], i.e. several satellites act together to achieve joint mission objectives.…”
Section: Introductionmentioning
confidence: 99%
“…Applications like weather monitoring and earth imaging clearly benefit from distributed approaches as well. An increasing number of space missions based on DSS is currently in various stages of development, most of them Earth science-related missions [6].…”
Section: Introductionmentioning
confidence: 99%
“…4,5 However, a survey of existing or proposed CubeSat FF missions concludes that there is a dearth of FF missions using four or more CubeSats that require formation maintenance and reconfiguration maneuvers. 6 Hence, the aim of this paper is to present a systems engineering based design of a formation flying technology demonstration mission using 4-6 CubeSats. The paper also highlights the (1a) 4 CubeSats maintain a tetrahedron formation in Low Earth Orbit (LEO) (1b) 6 CubeSats perform multiple optimal reconfiguration among different J2-invariant orbits.…”
Section: Introductionmentioning
confidence: 99%