Analysis on coupling model and mechanism of loop measurements in an ultra-tight GPS/INS integration
被引:0
作者:
Xie, Fei
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机构:
College of Automation, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaCollege of Automation, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Xie, Fei
[1
]
Liu, Jian-Ye
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机构:
College of Automation, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaCollege of Automation, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Liu, Jian-Ye
[1
]
Li, Rong-Bing
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机构:
College of Automation, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaCollege of Automation, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Li, Rong-Bing
[1
]
Han, Zhi-Feng
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机构:
College of Automation, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaCollege of Automation, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Han, Zhi-Feng
[1
]
机构:
[1] College of Automation, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Integration - Inertial navigation systems - Navigation;
D O I:
暂无
中图分类号:
O172 [微积分];
学科分类号:
摘要:
An ultra-tightly coupled model and a method for controlling replica signals generation in the tracking loop are proposed based on the analysis of various ultra-tight GPS/INS integration model. Moreover, the intrinsic relationships between the loop measurements and INS navigation solutions in an ultra-tight GPS/INS Integration model are analyzed and demonstrated. Finally, the coupling experiments are carried out, and the experiment results indicate that there is an intrinsic relationship and a deep fusion mechanism between tracking loop measurements and INS navigation solutions in an ultra-tight GPS/INS integration model.