Modeling of Dual-Spinning Projectile with Canard and Trajectory Filtering

被引:8
|
作者
Guan, Jun [1 ]
Yi, Wenjun [1 ]
机构
[1] Nanjing Univ Sci & Technol, Natl Key Lab Transient Phys, Nanjing 210094, Jiangsu, Peoples R China
基金
中国国家自然科学基金;
关键词
GUIDANCE; DESIGN;
D O I
10.1155/2018/1795158
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The article establishes a seven-degree-of-freedom projectile trajectory model for a new type of spinning projectile. Based on this model, a numerical analysis is performed on the ballistic characteristics of the projectile, and the trajectory of the dual-spinning projectile is filtered with the unscented Kalman filter algorithm, so that the measurement information of projectile onboard equipment is more accurate and more reliable measurement data are provided for the guidance system. The numerical simulation indicates that the dual-spinning projectile is mainly different from the traditional spinning projectile in that a degree of freedom is added in the direction of the axis of the projectile, the forebody of the projectile spins at a low speed or even holds still to improve the control precision of the projectile control system, while the afterbody spins at a high speed maintaining the gyroscopic stability of the projectile. The trajectory filtering performed according to the unscented Kalman filter algorithm can improve the accuracy of measurement data and eliminate the measurement error effectively, so as to obtain more accurate and reliable measurement data.
引用
收藏
页数:7
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