Satellite Attitude Control by Quaternion-Based Backstepping

Satellite Attitude Control by Quaternion-Based Backstepping

In this brief, a tracking controller is presented to stabilize the attitude of a micro satellite via integrator backstepping and quaternion feedback. The controller is shown to render the equilibrium points in the closed-loop system uniformly asymptotically stable. Simulations are performed using sa...

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Veröffentlicht in:IEEE transactions on control systems technology 2009-01, Vol.17 (1), p.227-232
Hauptverfasser: Kristiansen, R., Nicklasson, P.J., Gravdahl, J.T.
Format: Artikel
Sprache:eng
Schlagworte:
Applied sciences
Asymptotic properties
Attitude control
Backstepping
Computer science
control theory
systems
Control systems
Control theory
Control theory. Systems
Exact sciences and technology
Feedback
Fundamental areas of phenomenology (including applications)
integrator backstepping
Physics
Pulse width modulation
quaternion feedback
Quaternions
Satellites
Simulation
Solid dynamics (ballistics, collision, multibody system, stabilization...)
Solid mechanics
Space technology
space vehicle control
Space vehicles
Tracking
Weight control
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Beschreibung
Zusammenfassung:In this brief, a tracking controller is presented to stabilize the attitude of a micro satellite via integrator backstepping and quaternion feedback. The controller is shown to render the equilibrium points in the closed-loop system uniformly asymptotically stable. Simulations are performed using satellite parameters from the ESEO mission under the European Space Agency's SSETI project.
ISSN:1063-6536
1558-0865
DOI:10.1109/TCST.2008.924576