SIMULTANEOUS OPTIMUM DESIGN OF SHAPE AND CONTROL SYSTEM FOR MICRO AIR VEHICLES

SIMULTANEOUS OPTIMUM DESIGN OF SHAPE AND CONTROL SYSTEM FOR MICRO AIR VEHICLES
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微型飞行器外形与控制系统同步优化设计

DOI：
10.2514/6.1999-1391
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发表时间：
1999
期刊：
--
影响因子：
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通讯作者：
R. Haftka
R. Haftka
中科院分区：
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文献类型：
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作者：
I. Kajiwara;R. Haftka

文献摘要

被引文献

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微型飞行器（MAV）技术一直是研究人员关注的焦点。多学科优化有望帮助实现成功的mav所需的稳定性和更高的性能。本文论证了采用气动外形优化和控制系统设计相结合的方法来提高飞机的稳定性和性能。随着整车尺寸的日益小型化，侧倾运动的控制难度越来越大，优化的目标是减少控制能量，提高侧倾运动的控制稳定性。
Technology for micro air vehicles (MAV) has been attracting the attention of researchers. Multidisciplinary optimization is expected to help achieve the stability and higher performance required for successful MAVs. This paper demonstrates the use of simultaneous aerodynamic shape optimization and control system design for improved stability and performance. The objective of the optimization is to reduce the control energy and improve stability for controlling the roll motion, which becomes increasingly difficult to control as vehicle size gets smaller.