NASA NTRS · 19720032809
Absolute stability analysis of attitude control systems for large boosters.
Abstract
A method for performing an absolute stability analysis of attitude control systems for large launch vehicles is presented. Absolute stability of these systems is shown to be of a limited extent. The regions of absolute stability are computed by using a quadratic Liapunov function. The function is chosen to provide additional information about the exponential property of absolute stability. A system model is used to illustrate the method.
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Siljak, D. D., Seltzer, S. M.. 1971-01-01. Absolute stability analysis of attitude control systems for large boosters.. https://ntrs.nasa.gov/citations/19720032809
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