系统工程与电子技术 ›› 2023, Vol. 45 ›› Issue (1): 210-220.doi: 10.12305/j.issn.1001-506X.2023.01.25
• 制导、导航与控制 • 上一篇
高利春1,2,*, 高铭阳1, 陈晓芳2, 饶建兵1, 费泽松3, 倪少杰4
收稿日期:
2020-11-23
出版日期:
2023-01-01
发布日期:
2023-01-03
通讯作者:
高利春
作者简介:
高利春 (1984—), 男, 高级工程师, 博士研究生, 主要研究方向为卫星通信、管理科学与工程基金资助:
Lichun GAO1,2,*, Mingyang GAO1, Xiaofang CHEN2, Jianbing RAO1, Zesong FEI3, Shaojie NI4
Received:
2020-11-23
Online:
2023-01-01
Published:
2023-01-03
Contact:
Lichun GAO
摘要:
可重复使用运载器在进近着陆阶段对位置偏差有较高的精度要求, 而现有的组合导航方式的导航误差波动幅度较大, 难以满足运载器在进近着陆段的导航要求。因此,本文利用捷联惯导系统(strap-down inertial navigation system,SINS)的非线性误差传播模型, 以陆基增强系统(ground based augmentation system,GBAS)输出的精确位置信息为基础, 建立SINS/GBAS组合导航方法, 并给出“输出+反馈”的组合导航复合修正结构。通过在GBAS中引入电离层误差及对流层误差, 从而实现了对于运载器定位误差在厘米级的精确定位。此外,通过引入扩展卡尔曼滤波技术, 有效地抑制了惯导误差漂移的问题。通过数值模拟仿真, 证明SINS/GBAS组合导航对飞行器进近着陆段的水平与高程定位误差不大于0.05 m, 测速误差不大于0.05 m/s, 从而证实了SINS/GBAS组合导航方式在可重复运载器在进近着陆段导航的可行性。
中图分类号:
高利春, 高铭阳, 陈晓芳, 饶建兵, 费泽松, 倪少杰. 基于SINS/GBAS组合导航的高精度进近着陆导航技术[J]. 系统工程与电子技术, 2023, 45(1): 210-220.
Lichun GAO, Mingyang GAO, Xiaofang CHEN, Jianbing RAO, Zesong FEI, Shaojie NI. High precision approach-and-landing navigation technology based on SINS/GBAS integrated navigation[J]. Systems Engineering and Electronics, 2023, 45(1): 210-220.
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