NASA NTRS · 19740008449
Model-reference attitude control and reaction control jet engine placement for space shuttle
Abstract
Analytical studies on the theoretical aspects of thrust vector control of large space vehicles were conducted. A system for attitude control of the space shuttle vehicle was developed. Major accomplishments of the project are: (1) investigation of a model-reference adaptive control scheme for controlling the space shuttle attitude and (2) determination of optimum placement of reaction control jet engines on space shuttles.
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Boland, J. S., III. 1973-09-15. Model-reference attitude control and reaction control jet engine placement for space shuttle. https://ntrs.nasa.gov/citations/19740008449
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