摘要
针对变形翼飞行器变结构变形的特点,以某个变形翼飞行器的巡航和俯冲飞行模态作为研究对象,研究了两种模态下基于多控制器的去伪自适应控制技术和去伪控制算法,其中包括去伪控制器集和性能指标的确定等问题。最后在理论研究的基础上进行了仿真验证,仿真结果表明了去伪控制算法的可行性和有效性。
For variable structures of the morphing aircraft, specifically considering a transformation of morphing aircraft from loitering to diving, the unfalsified adaptive control techniques and algorithms based on multiple-controllers are studied. At the same time the set of controllers and the performance specification are determined. Then simulation and verification are conducted on the basis of theory study, and the results show the feasibility and effectiveness of the unfalsified control algorithm.
出处
《飞行力学》
CSCD
北大核心
2014年第6期514-517,共4页
Flight Dynamics
基金
国家自然科学基金资助(61074063)
关键词
变形翼飞行器
去伪控制
数据驱动
多控制器
morphing aircraft
unfalsified control
data driving
multiple-controllers
