OPTIMAL TAKEOFF PERFORMANCE OF A VECTORED THRUST AIRCRAFT

被引：0
|
作者：
AVANZINI, G
DEMATTEIS, G
机构：
来源：
AERONAUTICAL JOURNAL | 1995年 / 99卷 / 987期
关键词：
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The optimal takeoff performance of a vectored thrust V/Stol aircraft is analysed by a nonlinear programming method based on a sequential unconstrained minimisation technique. The study is focused on ship operations which involve VTO and ski-jump STO launches. Once the optimal ramp geometry is determined, minimum-fuel and minimum-time problems are solved. The optimal control sequences are evaluated and the effects of ship motion and atmospheric winds are discussed. A microburst encounter following an STO launch is also dealt with in terms of aircraft survival.
引用
收藏
页码：275 / 281
页数：7
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