摘要
针对四旋翼飞行器数学建模问题,分析系统运行过程中受力情况,探讨其动力学方程,并提出了基于此力学模型采用LQR控制方法实现对飞行器的控制,通过实时控制曲线,证实该方法的有效性和可行性。
According to four rotor aircraft mathematical modeling problem, this paper analyzes force situation in the process of system operation, and to explore its dynamic equation, and puts forward the LQR theory is adopted based on the mechanics model control method to achieve control of the aircraft through real-time control curve, confirmed the feasibility and effectiveness of the method.
出处
《机械管理开发》
2016年第10期1-2,23,共3页
Mechanical Management and Development
基金
2015年度湖南省教育厅科学研究项目(15C0903)--四旋翼飞行器的建模及控制策略的研究
