Spacecraft formation flying reconfiguration with extended and impulsive maneuvers

DOI10.1016/J.JFRANKLIN.2019.02.012zbMath1411.93127OpenAlexW2917523951MaRDI QIDQ1738624

Xianqiang Yang

Publication date: 18 April 2019

Published in: Journal of the Franklin Institute (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.jfranklin.2019.02.012

zbMATH Keywords

impulsive maneuversspacecraft formation flying reconfiguration

Mathematics Subject Classification ID

Application models in control theory (93C95)

Uses Software

• Optimization Toolbox

Cites Work

• Unnamed Item
• Analytic solution for fuel-optimal reconfiguration in relative motion
• Periodic motions
• Adaptive controller design for spacecraft formation flying using sliding mode controller and neural networks
• Coordinated orbit-tracking control of second-order non-linear agents with directed communication topologies
• Optimal Estimation of Dynamic Systems

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