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.
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.
出处
《飞行力学》
CSCD
北大核心
1992年第1期1-5,12,共6页
Flight Dynamics
关键词
舰载机
航迹
稳定性
直接升力控制
flight Path stability
unusual control range
active lift control
root path.
