摘要: The shuttle program took on the challenge of providing a manual landing capability for an operational vehicle returning from orbit. Some complex challenges were encountered in developing the longitudinal flying qualities required ... 展开
作者 | Powers, B. G. | ||
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原报告号 | N8510071 | 总页数 | 12 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Active control Flight characteristics Flight simulation Space shuttles Spacecraft landing Design analysis Flight control Flight tests Fly by wire control Oscillations Pilot performance Time lag |