Relative Motion Control For Two-Spacecraft Electrostatic Orbit Corrections

Author:

Hogan Erik A.1,Schaub Hanspeter1

Affiliation:

1. Aerospace Engineering Sciences, University of Colorado at Boulder, Boulder, Colorado 80309

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Reference13 articles.

1. KingL. B.ParkerG. G.DeshmukhS.ChongJ.H. “Spacecraft Formation-flying using Inter-vehicle Coulomb Forces,” NASA/NIAC, Technical Rept. http://www.niac.usra.edu, [retrieved Jan. 2002].

2. Study of Interspacecraft Coulomb Forces and Implications for Formation Flying

3. Hybrid control of orbit normal and along-track two-craft Coulomb tethers

4. Tethered Coulomb Structures: Prospects and Challenges

5. Nonlinear Charge Control for a Collinear Fixed-Shape Three-Craft Equilibrium

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