摘要
从气动和控制综合设计角度,提出了解决飞翼布局无人机稳定能力问题的多轴静不稳定增稳控制规律,通过对多操纵面操纵特性和操纵需求分析给出了操纵面的配置策略。仿真分析表明,所提出的设计方法较好地解决了飞翼布局无人机特殊的稳定与操纵问题。
In this paper,the designing method was analyzed in the level of the aerodynamics and flight control system synthesis.A control augmentation system was studied by analyzing the stable capability,and a control allocation strategy was presented according to the flying wing UAV with multi-effectors controllability and its control requirements.The result of simulation shows that the method paves a good way for successful control of the flying wing UAV with specific stability and controllability.
出处
《飞行力学》
CSCD
北大核心
2011年第1期9-12,共4页
Flight Dynamics
基金
国家"863"计划资助(863705705)
关键词
飞翼布局无人机
稳定与操纵
增稳控制
操纵面配置
flying wing UAV
stability and controllability
augmentation control
control allocation
