Evaluation of aircraft performance and maneuverability by computation of attainable equilibrium sets

被引：54

作者：

Goman, M. G. ^{[1
]}

Khramtsovsky, A. V. ^{[1
]}

Kolesnikov, E. N. ^{[1
]}

机构：

[1] De Montfort Univ, Fac Engn & Comp Sci, Leicester LE1 9BH, Leics, England

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2008年 / 31卷 / 02期

关键词：

D O I：

10.2514/1.29336

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

An aircraft's performance and maneuvering capabilities in steady flight conditions are usually analyzed considering the steady states of the rigid-body equations of motion. A systematic way of computation of the set of all attainable steady states for a general class of helical trajectories is presented. The proposed reconstruction of attainable equilibrium states and their local stability maps provides a comprehensive and consistent representation of the aircraft flight and maneuvering envelopes. The numerical procedure is outlined and computational examples of attainable equilibrium sets in the form of two-dimensional cross sections of steady-state maneuver parameters are presented for three different aircraft models.

引用

页码：329 / 339

页数：11

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