NASA NTRS · 19910065043
Dynamic attitude command and control of the TOPEX/Poseidon spacecraft
Abstract
The dynamic control laws utilized by the TOPEX/Poseidon (T/P) spacecraft attitude determination and control subsystem to command and maneuver the satellite during normal mission mode (NMM) laws are described. Results show that the vehicle is able to respond to the dynamic attitude commands while at the same time providing ample disturbance rejection capability.
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Zimbelman, D. F., Lee, B. B., Welch, R. V.. 1991-01-01. Dynamic attitude command and control of the TOPEX/Poseidon spacecraft. https://ntrs.nasa.gov/citations/19910065043
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