摘要: The Load Alleviation and Mode Stabilization (LAMS) program was conducted to demonstrate the capabilities of an advanced flight control system (FCS) to alleviate gust loads and control structural modes on a large flexible aircraft ... 展开
作者 | Burris, P. M. Bender, M. A. | ||
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原报告号 | AD864555 | 总页数 | 264 |
主办者 | Non Paid Delimited ADS | ||
报告分类号 | [51C - Aircraft] | ||
报告类别/文献类型 | AD / NTIS科技报告 | ||
关键词 | Jet bombers Flight control systems Jet transport planes Stabilization Gust loads Aerodynamic control surfaces Flight testing Fatigue(Mechanics) Damage Mathematical analysis Design Aircraft B-52e aircraft B-52 aircraft C-5 aircraft C-5a aircraft Fly by wire flight control systems Lams(Load alleviation and mode stabilization) Load alleviation and mode stabilization |