Explicit Dipole Trajectory Solution for Electromagnetically Controlled Spacecraft Clusters

Samuel A. Schweighart; Raymond J. Sedwick

doi:10.2514/1.46363

journal article Jul 01, 2010

Explicit Dipole Trajectory Solution for Electromagnetically Controlled Spacecraft Clusters

Samuel A. Schweighart Raymond J. Sedwick

Journal of Guidance, Control, and Dynamics Vol. 33 No. 4 pp. 1225-1235 · American Institute of Aeronautics and Astronautics (AIAA)

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References

Details

Published: Jul 01, 2010
Vol/Issue: 33(4)
Pages: 1225-1235

Authors

S

Samuel A. Schweighart

Massachusetts Institute of Technology, Cambridge, Massachusetts 02139

R

Raymond J. Sedwick

University of Maryland, College Park, Maryland 20742

Cite This Article

Samuel A. Schweighart, Raymond J. Sedwick (2010). Explicit Dipole Trajectory Solution for Electromagnetically Controlled Spacecraft Clusters. Journal of Guidance, Control, and Dynamics, 33(4), 1225-1235. https://doi.org/10.2514/1.46363

Explicit Dipole Trajectory Solution for Electromagnetically Controlled Spacecraft Clusters

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