摘要
将Hermite插值定理用于某远程多用途导弹捷联惯性导航系统的姿态解算 ,解决了弹体高动态特性与相对较低的传感器采样频率之间的矛盾 .对仿真结果进行了分析 ,为远程多用途导弹采用捷联惯导方案获取弹体信息并进行制导提供了可能性 .
Based on Hermite interpolation,a new altitude arithmetic algorithm for strapdown INS of a kind of a long range multi use missile is presented.The contradiction between the high dynamic characteristic of the missile and the relative low sampling frequency of sensors is solved by using this algorithm.Simulation results are analyzed,thus makes it possible to take strapdown INS to measure altitudes for long range multi use missile in practice.
出处
《战术导弹技术》
2002年第1期31-33,共3页
Tactical Missile Technology
