摘要: An integrated methodology for propulsion and airframe control has been developedand evaluated for a Short Take-Off Vertical Landing (STOVL) aircraft using a fixed base flight simulator at NASA Lewis Research Center. For this evalu... 展开
作者 | Bright, M. M. Simon, D. L. Garg, S. Mattern, D. L. Ranaudo, R. J. | ||
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原报告号 | N9512763 | 总页数 | 14 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Aircraft control Control simulation Control systems design Flight control Flight simulation Stovl aircraft Thrust control Cockpits Display devices Flight paths Flight simulators Transition flight Turbofan engines |