| 直接升力控制对飞机着舰稳定性的改善 |
| |
| 引用本文： | 林国锋 高浩. 直接升力控制对飞机着舰稳定性的改善[J]. 飞行力学, 1992, 10(1): 1-5,12 |
| |
| 作者姓名： | 林国锋 高浩 |
| |
| 作者单位： | 西北工业大学，西北工业大学 |
| |
| 摘 要： | 本文讨论了舰载飞机以最小需用推力对应速度(V_(?))的左侧速度进场的航迹稳定性问题。并对直接升力控制对着舰稳定性的改善进行了初步探讨.结果表明,采用直接升力控制来保证飞机着舰稳定性是可行的.
|
| 关 键 词： | 舰载机 航迹 稳定性 直接升力控制 |
THE IMPROVEMENT IN FLIGHT PATH STABILITY OF SEA-BASED AIRCRAFT BY USING ACTIVE LIFT CONTROL |
| |
| Lin Guofeng,Gao Hao. THE IMPROVEMENT IN FLIGHT PATH STABILITY OF SEA-BASED AIRCRAFT BY USING ACTIVE LIFT CONTROL[J]. Flight Dynamics, 1992, 10(1): 1-5,12 |
| |
| Authors: | Lin Guofeng Gao Hao |
| |
| Affiliation: | Northwestern Polytechnical University |
| |
| Abstract: | In this paper, the landing approach flight path stability of sea-based aircraft at the speed less than that corresponding to minimum drag has been discussed. The improvement in this stability by using active lift control has also been studied. The result shows that improving the flight path stability by using active lift control is feasible. |
| |
| Keywords: | flight Path stability unusual control range active lift control root path. |
| 本文献已被 CNKI 维普 等数据库收录！ |
