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In Systems and Control in Aerospace and Astronautics, 2008. ISSCAA 2008. 2nd International Symposium on (December 2008), pp. 1-6, doi:10.1109/isscaa.2008.4776240 Key: citeulike:11962049
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The benefits of relaxed static stability on missile were examined. Based on optimal control and open-loop crossover frequency constraint, an acceleration autopilot design methodology was developed and applied to a highly unstable airframe. Performance and robustness comparisons for three autopilot topologies were made. The analysis reveals the topology origin of classic three-loop autopilot, and simulation results show that the four-loop topology looks very promising.
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