Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
698007 | Automatica | 2008 | 6 Pages |
Abstract
In this paper, we present three nonlinear control solutions for 6DOF spacecraft formation control, adopted from Euler–Lagrange system theory. The quaternion parametrization results in dual equilibrium points in the closed loop system, and the controllers are proved to render these uniformly asymptotically stable. We also present a theoretical comparison of the three control solutions, together with simulation results to visualize the performance of the controllers.
Keywords
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Physical Sciences and Engineering
Engineering
Control and Systems Engineering
Authors
Raymond Kristiansen, Per Johan Nicklasson, Jan Tommy Gravdahl,