摘要
提出了一种小型无人机平尾多目标优化方法。在保证飞行品质的前提下,实现了平尾阻力和尾撑结构质量最小的优化目标。通过优化,无人机纵向静稳定性降低,纵向操纵性得到提高。该方法对小型无人机平尾设计具有一定借鉴意义。
A multi-objective optimization method was advanced to make the drag and structure mass minimum of horizontal stabilizer based the precondition of meeting flying qualities. After the optimization, the longitudinal stability reduced, the longitudinal control performance increased. This method has refer- ential meaning for the design of horizontal stabilizer for Mini-UVA.
出处
《宇航计测技术》
CSCD
2013年第4期62-64,78,共4页
Journal of Astronautic Metrology and Measurement
关键词
无人机
平尾
优化设计
UVA Horizontal stabilizer Optimization design
