变形
航空航天工程
飞行操纵面
比例(比率)
计算机科学
空气动力学
飞机
飞机飞行力学
航空学
飞行动力学
环境科学
工程类
物理
计算机视觉
量子力学
作者
Thomas M. Seigler,David A. Neal,Jae-Sung Bae,Daniel J. Inman
出处
期刊:Journal of Aircraft
[American Institute of Aeronautics and Astronautics]
日期:2007-07-01
卷期号:44 (4): 1077-1087
被引量:139
摘要
As morphing is an emerging topic of interest in aircraft research, the following article provides a review of the subject, with specific focus on modeling and flight control of large-scale planform altering flight vehicles. Our discussion proceeds in a fundamental manner to demonstrate that, although design methods for rigid aircraft have become highly developed, the consideration of morphing necessitates further investigation into the typically disparate fields of dynamic modeling, aerodynamic theory, and flight control theory. To clarify these points, the equations of atmospheric flight are derived in a general form, methods of integrating the aerodynamic forces are examined, and we distinguish between various approaches and methods of flight control.
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