Finite-time control of underactuated spacecraft hovering

Author:

Huang Xu,Yan Ye,Huang Zherui

Funder

National Natural Science Foundation of China

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

Hunan Provincial Innovation Foundation

Publisher

Elsevier BV

Subject

Applied Mathematics,Electrical and Electronic Engineering,Computer Science Applications,Control and Systems Engineering

Reference50 articles.

1. Rendezvous maneuvers of multiple spacecraft using differential drag under J2 perturbation;Bevilacqua;Journal of Guidance, Control, and Dynamics,2008

2. Control of hovering spacecraft near small bodies: application to asteroid 25143 Itokawa;Broschart;Journal of Guidance, Control, and Dynamics,2005

3. Boundedness of spacecraft hovering under dead-band control in time-invariant systems;Broschart;Journal of Guidance, Control, and Dynamics,2007

4. Terminal guidance system for satellite rendezvous;Clohessy;Journal of Aerospace Science,1960

5. Modeling and analysis of relative hovering control for spacecraft;Dang;Journal of Guidance, Control, and Dynamics,2014

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