AIRCRAFT MODEL FOR THE AIAA CONTROLS DESIGN CHALLENGE

被引：13

作者：

BRUMBAUGH, RW

机构：

[1] PRC Inc, Edwards, CA

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 1994年 / 17卷 / 04期

关键词：

D O I：

10.2514/3.21263

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper describes a generic, state-of-the-art, high-performance aircraft model, including detailed, full-envelope, nonlinear aerodynamics, and full-envelope thrust and first-order engine response data. Although this model was developed primarily for the AIAA Controls Design Challenge, the availability of such a model provides a common focus for research in aeronautical control theory and methodology. Figures showing vehicle geometry, surfaces, and sign conventions are included.

引用

页码：747 / 752

页数：6