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固体运载火箭捷联惯导快速水平对准研究
任玉川,蔡虹曼,邵会兵
0
(北京控制与电子技术研究所)
摘要:
传统的水平对准由于采用了复杂的滤波环节,需要较长的时间来完成水平对准工作,难以满足固体运载火箭捷联惯导快速水平对准的需求。为了满足固体运载火箭的快速发射需求,研究了一种基于导航方式的快速水平对准方法,仿真结果表明,该方法能够在〖WTBZ〗15s内完成捷联惯导的水平对准工作,并且能够克服运载火箭扰动环境对水平对准精度的影响。
关键词:  固体运载火箭  捷联惯导  水平对准
DOI:
基金项目:
Research on Rapid Horizontal Alignment of Strap-down Inertial Navigation System on Solid Launch Vehicle
REN Yu-chuan,CAI Hong-man,SHAO Hui-bing
(China Beijing Institute of Control & Electronic Technology)
Abstract:
Usually, complicated filter algorithm is adopted by the traditional horizontal alignment, which can not meet the rapid launching requirement of solid launch vehicle In order to meet the rapid launching requirement of solid launch vehicle, a rapid horizontal alignment algorithm based on navigation is presented The simulation results show that, by using this method, the inertial navigation system on the solid launch vehicle can finish horizontal alignment in less than 15 seconds Also, this method is suitable for the shake environment of solid launch vehicle.
Key words:  Solid launch vehicle  Strap-down inertial navigation system  Horizontal alignment

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