2016
DOI: 10.2514/1.a33291
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Review of Formation Flying and Constellation Missions Using Nanosatellites

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Cited by 191 publications
(88 citation statements)
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“…The aforementioned conditions are conclusive in the absence of other dynamical terms like (4). The passivity of the input-output dynamics [67]- [69] is commonly used to analyze the stability of networked nonlinear systems that have both the Laplacian matrix (L in (4)) and the nonlinear dynamical terms (e.g., convection terms of (3) or the Lagrangian form in (5)).…”
Section: F Synchronization and Hierarchical Stability For Swarmsmentioning
confidence: 99%
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“…The aforementioned conditions are conclusive in the absence of other dynamical terms like (4). The passivity of the input-output dynamics [67]- [69] is commonly used to analyze the stability of networked nonlinear systems that have both the Laplacian matrix (L in (4)) and the nonlinear dynamical terms (e.g., convection terms of (3) or the Lagrangian form in (5)).…”
Section: F Synchronization and Hierarchical Stability For Swarmsmentioning
confidence: 99%
“…If a linear diffusive coupling is used, τ i would produce L similar to (4). The EulerLagrange equations appear routinely robotics in the study of rigid body motions of manipulators [26], [27] and spacecraft or aircraft (SE(3)), which have attitude dynamics on SO(3) [28]- [30] and often times have articulated wings [14], [31], [32], appendages, or manipulators attached:…”
Section: Physics-based Models For Robotic Agentsmentioning
confidence: 99%
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“…[2][3][4][5][6][7] Although there have been significant advances in the development of swarm guidance algorithms for cooperative spacecraft, they cannot be directly applied to handle static and time-varying uncooperative obstacles. In this paper, we present a novel guidance algorithm for spacecraft swarms in an active environment cluttered with many time-varying, moving obstacles, like a debris field or the asteroid belt, and desired time-varying terminal positions.…”
Section: Introductionmentioning
confidence: 99%
“…This increase in the last years of science missions in LEO orbits can be seen in; small satellites projects which integrate CubeSat platform units, such as FIREBIRD placed into orbit by the Delta II rocket to study the Van Allen belts radiation (Crew et al 2015), and Centennial placed into orbit by the ISS to validate a satellite monitoring system from Earth; initiatives of CubeSat constellations (Conklin et al 2013;Leiter, 2013;Subramanian et al 2015;Peral et al 2015;Bandyopadhyay et al 2016), and; experimental studies in CubeSat performances and specific applications (Jones, 2013;Cartwright, 2014;Venturini, 2014;Briggs et al 2015;Fields et al 2015;Westerhoff et al 2015;Carreno-Luengo et al 2016). In addition, the last report …”
Section: Leo Orbits Missionsmentioning
confidence: 99%