摘要
小型四旋翼飞行器在民用与军事等各个领域具有广泛应用,是当前研究的热点之一。四旋翼稳定与可靠飞行的前提必须依靠迅速和精确的姿态角数据解算。因为姿态角解算精确程度直接影响着四旋翼飞行器在飞行过程中的灵活性、稳定性、抗干扰性,所以对姿态角解算方法的研究具有重大意义。
The small quad-rotor aircraft has been widely used in various fields, such as civil and military, and is one of the hot spots of current research. The quadrotors can be stable and reliable flight conditions must rely on rapid and accurate angular data solutions. Because of the attitude Angle calculating accuracy directly affects the four rotor aircraft in flight process flexibility, stability and anti- interference, so the study of attitude Angle calculating method is of great significance.
作者
刘晓宇
孟瑞锋
贾伟
Liu Xiaoyu;Meng Ruifeng;Jia Wei(Inner Mongolia university of technology institute of mechanical,Inner Mongolia Hohhot 010051)
