Piloted simulation tools for aircraft departure analysis

被引：4

作者：

Patel, Y ^{[1
]}

Littleboy, D ^{[1
]}

机构：

[1] Def Evaluat & Res Agcy, Bedford MK41 6AE, England

来源：

PHILOSOPHICAL TRANSACTIONS OF THE ROYAL SOCIETY A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES | 1998年 / 356卷 / 1745期

关键词：

departure prediction; bifurcation analysis; piloted simulation; combat aircraft;

D O I：

10.1098/rsta.1998.0270

中图分类号：

O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];

学科分类号：

07 ; 0710 ; 09 ;

摘要：

This paper presents the piloted simulation tools and methods used on the Defence Evaluation and Research Agency (Bedford) flight simulators to investigate departures predicted by theoretical bifurcation analysis. In particular, the use of head down displays showing bifurcation diagrams, nonlinear dynamic inversion control; specific piloting approaches and 'spin templates' to classify departure modes is described. Piloted simulation time histories for autorotation, upright spins and deep stall of various aircraft are also presented. The paper concludes with recommendations on the 'optimum' combination of theoretical analysis and piloted simulation for complete departure analysis.

引用

页码：2203 / 2221

页数：19

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