摘要: A multivariable error-actuated digital tracking controller is developed for the Mach 0.18 flight condition of the A-7D Digitac II aircraft using a singular perturbation method. The design is accomplished and simulated after the de... 展开
作者 | Porter, D. S. | ||
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原报告号 | AD-A118134 | 总页数 | 106 |
报告类别/文献类型 | AD / NTIS科技报告 | ||
关键词 | Flight control systems Control theory Computer aided design Fighter aircraft Attack aircraft Computer programs Interactions Aircraft models Degrees of freedom Multivariate analysis Digital systems user manuals Programming manuals Theses Perturbation |