NASA NTRS · 19720003296
Development of control systems for space shuttle vehicles, volume 1
Abstract
Control of winged two-stage space shuttle vehicles was investigated. Control requirements were determined and systems capable of meeting these requirements were synthesized. Control requirements unique to shuttles were identified. It is shown that these requirements can be satisfied by conventional control logics. Linear gain schedule controllers predominate. Actuator saturations require nonlinear compensation in some of the control systems.
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Stone, C. R., Chase, T. W., Kiziloz, B. M., Skelley, E. D., Stein, G., Ward, M. D., Skelton, G. B., Yore, E. E., Rupert, J. G., Phelps, R. K.. 1971-10-01. Development of control systems for space shuttle vehicles, volume 1. https://ntrs.nasa.gov/citations/19720003296
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