Output feedback control of Lorentz-augmented spacecraft rendezvous-Reference-Cited by-同舟云学术

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Output feedback control of Lorentz-augmented spacecraft rendezvous

Published:2015-04 Issue: Volume:42 Page:241-248
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Huang Xu,Yan Ye,Zhou Yang,Yu Jinlong

Funder

Fund of Innovation by Graduate School of National University of Defense Technology

Hunan Provincial Innovation Foundation

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference21 articles.

1. Direct trajectory optimization and costate estimation via an orthogonal collocation method;Benson;J. Guid. Control Dyn.,2006

2. Propellantless stationkeeping at Enceladus via the electromagnetic Lorentz force;Gangestad;J. Guid. Control Dyn.,2009

3. Lagrange's planetary equations for the motion of electrostatically charged spacecraft;Gangestad;Celest. Mech. Dyn. Astron.,2010

4. Analytical expressions that characterize propellantless capture with electrostatically charged spacecraft;Gangestad;J. Guid. Control Dyn.,2011

5. Dynamics and control of spacecraft hovering using the geomagnetic Lorentz force;Huang;Adv. Space Res.,2014

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1. Optimal spacecraft rendezvous using the combination of aerodynamic force and Lorentz force;Advances in Space Research;2021-06

2. Spacecraft formation control using aerodynamic and Lorentz force;Aircraft Engineering and Aerospace Technology;2020-03-18

3. Minimum-Learning-Parameter-Based Fault-Tolerant Control for Spacecraft Rendezvous With Unknown Inertial Parameters;IEEE Access;2020

4. Output feedback robust H∞ control for spacecraft rendezvous system subject to input saturation: A gain scheduled approach;Journal of the Franklin Institute;2019-05

5. Stabilization of a programmed rotation mode for a satellite with electrodynamic attitude control system;Advances in Space Research;2018-07

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