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SINS and Aiming-Line Error Model for a Small Tactical Missile
Author(s): 
Pages: 949-952
Year: Issue:  11
Journal: Transactions of Beijing Institute of Technology

Keyword:  捷联惯导数学平台瞄准线转动误差;
Abstract: 为了系统地研究小型战术导弹捷联惯导系统的误差特性,在初始对准数学模型的基础上利用坐标变换和相似变换原理,建立了捷联惯导系统数学平台漂移模型、加速度误差模型和瞄准线转动误差模型,并对模型进行了分析.通过仿真实验验证了模型的正确性和可行性,给出了满足要求的惯性器件精度.
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