摘要: Advanced flight control system design, analysis, and testing methods are applied in an analytical and flight test evaluation of the Advanced Digital Optical Control System (ADOCS) demonstrator. This paper describes the knowledge g... 展开
作者 | Tischler, M. B. Fletcher, J. W. Morris, P. M. Tucker, G. T. | ||
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原报告号 | ADA211906 | 总页数 | 62 |
主办者 | Army Non Paid ADAS | ||
报告分类号 | [51E - Avionics, 51C - Aircraft] | ||
报告类别/文献类型 | AD / NTIS科技报告 | ||
关键词 | Flight control systems Rotary wing aircraft Actuators Aerodynamic characteristics Bandwidth Boundaries Correlation Damping Delay Digital systems Extraction Flight testing Frequency Handling High gain Aircraft landings Mathematical models Military aircraft Optical equipment Phase Pilots Rates Response Specifications Test and evaluation Test methods Warfare ADOCS(Advanced Digital Optical Control System) Digital flight control Handling qualities Ultrahigh gain |