大气高度辅助的惯导/SAR组合自适应算法研究

Adaptive Fiter Algorithm of Ins/Sar Intergrated Navigation Based on Barometric Altimeter

在组合惯导系统优化问题的研究中,SAR图像匹配导航仅能提供对惯性导航误差水平位置修正,无法获得高度信息。为改善基于经典控制理论设计的惯性/大气阻尼高度通道性能,充分体现大气和惯性导航两者结合的优势,提出了利用大气高度辅助惯性/SAR的组合导航方案。在深入分析惯性/大气高度阻尼系统工作原理的基础上,设计了考虑大气动态测量误差的组合模型;为有效提升组合系统在跨音速等高动态飞行条件下的导航性能,提出了改进的采用大气高度辅助的惯导/SAR组合自适应Sage-Husa方法。最后仿真可行性结果表明,提出的大气高度辅助的惯导/SAR自适应组合滤波方法可以有效改善跨音速等高动态环境下的组合系统性能。

Consider the shortcoming that SAR image matching navigation can only provide inertial navigation error level position correction ; in order to improve the classical control theory design inertia/air damper height channel performanee, fully reflect both the atmosphere and inertial navigation union performance advantage, we studied and put forward an integrated navigation scheme using atmospheric altitude auxiliary INS/SAR. The paper designed atmosphere combination model considering dynamic measurement error based on thorough analysis of the basic principle of the inertia/air altitude damping system. To enhance the combination system in transonic flight dynamic flight conditions navigation performance, the paper put forward the atmospheric height of auxiliary based on inertial navigation/ SAR combination adaptive Sage - Husa method. Integrated navigation system simulation results show that the proposed adaptive filter algorithm of INS/SAR can effectively improve transonic flight dynamic environment combination system performance, so as provides a good way to solve the inertial/SAR combination altitude channel stable performance.