Optimal Attitude Control of a 6U CubeSat with a Four-Wheel Pyramid Reaction Wheel Array and Magnetic Torque Coils

Authors

Kerianne H. Gross, Air Force Research Laboratory
Ryan M. Patrick, Air Force Institute of Technology
Eric D. Swenson, Air Force Institute of Technology
Jeremy S. Agte, AFMC 96th OG Det 2

Document Type

Conference Proceeding

Publication Date

1-4-2016

Comments

Session: Special Topics in Modeling and Simulation

Author note: Ryan Patrick was an AFIT graduate student (M.S.) at the time of this conference. (AFIT-ENY-MS-16-M-232, March 2016)

This conference paper is published by AIAA and is available by subscription or purchase at the DOI link below.

DOI

10.2514/6.2016-0174

Source Publication

AIAA Modeling and Simulation Technologies Conference

Recommended Citation

Gross, K. H., Patrick, R., Swenson, E. D., & Agte, J. S. (2016, January). Optimal Attitude Control of a 6U CubeSat with a Four-Wheel Pyramid Reaction Wheel Array and Magnetic Torque Coils. AIAA Modeling and Simulation Technologies Conference. https://doi.org/10.2514/6.2016-0174