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Satellite Formation-Containment Flying Control with Collision Avoidance
Journal of Aerospace Information Systems, 2018This paper investigates the satellite formation-containment flying control problem to handle a scenario where a group of satellite effectively completes deep-space exploration.
Liangming Chen +2 more
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Agent Based Controller for Satellite Formation Flying
In this paper an agent based control scheme for satellite formation flying is discussed. The underlying idea of our design is to use a multi-agent architecture for satellite formation flying control. The architecture is designed to enable autonomous formation flying activities. The performance requirements and algorithms are described.
K.K.T. Thanapalan, S.M. Veres
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Satellite affine formation flying with obstacle avoidance
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2019This paper studies the affine formation control problem for a group of flying satellites with the performance of obstacle avoidance. Assuming that leader satellites can detect the locations of obstacles, we first investigate how to plan advisable trajectories for leader satellites such that they can smoothly pass through some specific types of ...
Liangming Chen +2 more
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Formation Flying Satellites: Control By an Astrodynamicist
Celestial Mechanics and Dynamical Astronomy, 2001Potential periodic formation orbits can be identified using Hill's equation. However, as gravitational perturbations destroy the periodicity, a control is required to maintain the desired orbits. Here, the authors address the control of individual satellites as well as the control of the whole constellation.
Alfriend, Kyle T. +2 more
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Optimal Reconfiguration of Formation Flying Satellites
Proceedings of the 44th IEEE Conference on Decision and Control, 2006We employ a recently developed new technique for the numerical treatment of optimal control problems for mechanical systems in order to compute optimal open loop control laws for the reconfiguration of a group of formation flying satellites. The method is based on a direct discretization of a variational formulation of the dynamical constraints.
Oliver Junge, Sina Ober-Blöbaum
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Ultra-Dense LEO Satellite Based Formation Flying
IEEE Transactions on Communications, 2021In this article, we consider a downlink ultra-dense LEO-based multi-terminal satellite system where multiple satellites fly in formation to serve a number of ground terminal stations for data transmission. Benefited from the dense satellite constellation, high channel capacity can be achieved via the massive virtual antenna array formed by multiple ...
Ruoqi Deng, Boya Di, Lingyang Song
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Adaptive control for satellite formation flying under thrust misalignment
Satellite formation flying requires precise control of relative positioning under external disturbances and parameter uncertainties. Since thrust magnitude error and misalignment are not negligible in the electric propulsion system, they should be ...
Hyung-Chul Lim, Hyochoong Bang
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On the formation flying of satellite constellations
Chinese Astronomy and Astrophysics, 2004Abstract From the viewpoint of orbit dynamics, the formation flying of the satellites of a constellation and the accompanying flying in satellite-satellite tracking are affected by the following dynamical mechanisms: (1) The main characteristics of the variations of disturbed orbits determine the space configuration of the satellites.
Lin Liu, Hai-hong Wang, Jian-bo Ma
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Cooperative fault accommodation in formation flying satellites
2008 IEEE International Conference on Control Applications, 2008In this paper a new fault accommodation algorithm based on a two-level architecture is proposed for satellite formation missions. In this two-level framework, the notion of formation-level fault recovery (FLFR) is proposed, and the task of performance monitoring (PM) is defined in the high level (HL). By using the information provided by the PM module,
Seyyedmohsen Azizi, Khashayar Khorasani
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An intelligent control concept for formation flying satellites
International Journal of Robust and Nonlinear Control, 2002AbstractThis paper deals with the determination of initial conditions and the design of fuel‐balancing orbit control laws for a formation of satellites. Hill's equations describe the linearized dynamics of relative motion between two satellites. They admit bounded relative orbit solutions as special cases.
Vadali, S. R. +2 more
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