NASA NTRS · 19800005912
Torque equilibrium attitude control for Skylab reentry
Abstract
All the available torque equilibrium attitudes (most were useless from the standpoint of lack of electrical power) and the equilibrium seeking method are presented, as well as the actual successful application during the 3 weeks prior to Skylab reentry.
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Glaese, J. R., Kennel, H. F.. 1979-11-01. Torque equilibrium attitude control for Skylab reentry. https://ntrs.nasa.gov/citations/19800005912
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