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https://doi.org/10.1016/b978-0-08-041715-8.50073-0
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Cite Journal: Automatic Control in Aerospace 1992 |  Publication Date: Jan 1, 1993 |
A non linear attitude control law has been synthesised for the early reentry trajectory of a space plane, in the transition domain corresponding to low dynamic pressure, where it is necessary to pass from full thruster control to full aerodynamic control.
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