The dynamics and control of the CubeSail mission: A solar sailing demonstration

Andrew Pukniel, Victoria Coverstone, Rodney Burton, David Carroll

Research output: Contribution to journalArticle

10 Scopus citations

Abstract

The CubeSail mission is a low-cost demonstration of the UltraSail solar sailing concept (Burton et al.; 2005; Botter et al.; 2006; Hargens-Rysanek, 2006; Pukniel, 2009), using two near-identical CubeSat satellites to deploy a 260 m-long, 20 m 2 reflecting film. The two satellites are launched as a unit, detumbled, and separated, with the film unwinding symmetrically from motorized reels. The conformity to the CubeSat specification allows for reduction in launch costs as a secondary payload and utilization of the University of Illinois-developed spacecraft bus. The CubeSail demonstration is the first in a series of increasingly-complex missions aimed at validating several spacecraft subsystems, including attitude determination and control, the separation release unit, reel-based film deployment, as well as the dynamical behavior of the sail and on-orbit solar propulsion. The presented work describes dynamical behavior and control methods used during three main phases of the mission. The three phases include initial detumbling and stabilization using magnetic torque actuators, gravity-gradient-based deployment of the film, and steady-state film deformations in low Earth orbit in the presence of external forces of solar radiation pressure, aerodynamic drag, and gravity-gradient.

Original languageEnglish (US)
Pages (from-to)1902-1910
Number of pages9
JournalAdvances in Space Research
Volume48
Issue number11
DOIs
StatePublished - Dec 1 2011
Externally publishedYes

Keywords

  • Low earth orbit missions
  • Mission design
  • Solar sailing
  • Spacecraft dynamics
  • Tether dynamics

ASJC Scopus subject areas

  • Aerospace Engineering
  • Astronomy and Astrophysics
  • Geophysics
  • Atmospheric Science
  • Space and Planetary Science
  • Earth and Planetary Sciences(all)

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