Title
Spacecraft coordination control in 6DOF: Integrator backstepping vs passivity-based control
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.
Year
DOI
Venue
2008
10.1016/j.automatica.2008.04.019
Automatica
Keywords
Field
DocType
Spacecraft control,Formation flying,Passivity-based control,Sliding surface,Backstepping design
Lyapunov function,Mathematical optimization,Backstepping,Nonlinear control,Control theory,Quaternion,Equilibrium point,Integrator,Exponential stability,Mathematics,Spacecraft
Journal
Volume
Issue
ISSN
44
11
0005-1098
Citations 
PageRank 
References 
18
1.50
2
Authors
3
Name
Order
Citations
PageRank
Raymond Kristiansen19616.09
Per Johan Nicklasson212920.47
Jan Tommy Gravdahl332743.60