CAJ | 학술논문

为了提高某型无人机飞行安全性和生存能力,基于模型跟随法设计了某型无人机方向舵卡死自修复控制律模型.分别对方向舵卡死故障模型及自修复模型进行了仿真,利用仿真结果对比分析了自修复前后无人机飞行状态.结果表明,通过设计的模型可以实现方向舵卡死的自修复控制,从而提高某型无人机飞控系统的可靠性和安全性.
위료제고모형무인궤비행안전성화생존능력,기우모형근수법설계료모형무인궤방향타잡사자수복공제률모형.분별대방향타잡사고장모형급자수복모형진행료방진,이용방진결과대비분석료자수복전후무인궤비행상태.결과표명,통과설계적모형가이실현방향타잡사적자수복공제,종이제고모형무인궤비공계통적가고성화안전성.
In order to improve the UAV flight safety and survival ability,the UAV rudder deadlock self?repairing control law model was designed based on the model following method. The rudder deadlock fault model and self?repairing model were simulated;UAV flight states before and after self?reparing were analyzed according to the simulation results. The results show that the rudder deadlock self?repairing control can be realized by using the model designed in this paper. Thereby the UAV flight control system reliability and safety can be improved.