航空兵器Issue(2)：29-31,3.DOI:10.19297/j.cnki.41-1228/tj.2016.02.005
基于机载捷联惯导计算导弹初始姿态的算法
Initial Attitude Algorithm of Missile Based on Airborne SINS
陈宇 1付书堂 1刘建团2
作者信息
- 1. 中国空空导弹研究院，河南洛阳 471009
- 2. 陆军航空局驻洛阳地区军事代表室，河南洛阳 471009
- 折叠
摘要
Abstract
With the development of inertial navigation technology, airborne platform inertial naviga-tion system is substituted gradually by SINS, which causes the change of missile attitude algorithm calcu-lated by fire control system.Research on the inertial navigation system algorithm is done and the attitude algorithm base on airborne SINS is summarized.The calculation accuracy of the algorithm meets the re-quirement and it can be used in the initialization of air-to-air missile navigation system.关键词
空空导弹/捷联惯导/初始校准/导弹姿态/算法设计Key words
air-to-air missile/SINS/initial alignment/missile attitude/algorithm design分类
航空航天引用本文复制引用
陈宇,付书堂,刘建团..基于机载捷联惯导计算导弹初始姿态的算法[J].航空兵器,2016,(2):29-31,3.
