An Optimization-Based Initial Alignment and Calibration Algorithm of Land-Vehicle SINS In-Motion
被引:9
作者:
Gao, Kang
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Harbin Inst Technol, Space Control & Inertial Technol Res Ctr, Harbin 150080, Heilongjiang, Peoples R ChinaHarbin Inst Technol, Space Control & Inertial Technol Res Ctr, Harbin 150080, Heilongjiang, Peoples R China
Gao, Kang
[1
]
Ren, Shunqing
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机构:
Harbin Inst Technol, Space Control & Inertial Technol Res Ctr, Harbin 150080, Heilongjiang, Peoples R ChinaHarbin Inst Technol, Space Control & Inertial Technol Res Ctr, Harbin 150080, Heilongjiang, Peoples R China
Ren, Shunqing
[1
]
Chen, Xijun
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机构:
Harbin Inst Technol, Space Control & Inertial Technol Res Ctr, Harbin 150080, Heilongjiang, Peoples R ChinaHarbin Inst Technol, Space Control & Inertial Technol Res Ctr, Harbin 150080, Heilongjiang, Peoples R China
Chen, Xijun
[1
]
Wang, Zhenhuan
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Harbin Inst Technol, Space Control & Inertial Technol Res Ctr, Harbin 150080, Heilongjiang, Peoples R ChinaHarbin Inst Technol, Space Control & Inertial Technol Res Ctr, Harbin 150080, Heilongjiang, Peoples R China
Wang, Zhenhuan
[1
]
机构:
[1] Harbin Inst Technol, Space Control & Inertial Technol Res Ctr, Harbin 150080, Heilongjiang, Peoples R China
For a running freely land-vehicle strapdown inertial navigation system (SINS), the problems of self-calibration and attitude alignment need to be solved simultaneously. This paper proposes a complete alignment algorithm for the land vehicle navigation using Inertial Measurement Units (IMUs) and an odometer. A self-calibration algorithm is proposed based on the global observability analysis to calibrate the odometer scale factor and IMU misalignment angle, and the initial alignment and calibration method based on optimal algorithm is established to estimate the attitude and other system parameters. This new algorithm has the capability of self-initialization and calibration without any prior attitude and sensor noise information. Computer simulation results show that the performance of the proposed algorithm is superior to the extended Kalman filter (EKF) method during the oscillating attitude motions, and the vehicle test validates its advantages.
机构:
China Univ Min & Technol, Sch Environm Sci & Spatial Informat, Xuzhou, Peoples R China
Xian Res Inst Surveying & Mapping, Xian, Peoples R ChinaChina Univ Min & Technol, Sch Environm Sci & Spatial Informat, Xuzhou, Peoples R China
机构:
Queens Univ, Dept Elect & Comp Engn, NavINST Nav & Instrumentat Res Grp, Kingston, ON, CanadaTrusted Positioning Inc, Calgary, AB, Canada
Karamat, Tashfeen
;
Iqbal, Umar
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机构:
Queens Univ, Dept Elect & Comp Engn, NavINST Nav & Instrumentat Res Grp, Kingston, ON, CanadaTrusted Positioning Inc, Calgary, AB, Canada
Iqbal, Umar
;
Noureldin, Aboelmagd
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机构:
Queens Univ, Dept Elect & Comp Engn, NavINST Nav & Instrumentat Res Grp, Kingston, ON, Canada
Royal Mil Coll Canada, Dept Elect & Comp Engn, NavINST Nav & Instrumentat Res Grp, Kingston, ON, CanadaTrusted Positioning Inc, Calgary, AB, Canada
机构:
China Univ Min & Technol, Sch Environm Sci & Spatial Informat, Xuzhou, Peoples R China
Xian Res Inst Surveying & Mapping, Xian, Peoples R ChinaChina Univ Min & Technol, Sch Environm Sci & Spatial Informat, Xuzhou, Peoples R China
机构:
Queens Univ, Dept Elect & Comp Engn, NavINST Nav & Instrumentat Res Grp, Kingston, ON, CanadaTrusted Positioning Inc, Calgary, AB, Canada
Karamat, Tashfeen
;
Iqbal, Umar
论文数: 0引用数: 0
h-index: 0
机构:
Queens Univ, Dept Elect & Comp Engn, NavINST Nav & Instrumentat Res Grp, Kingston, ON, CanadaTrusted Positioning Inc, Calgary, AB, Canada
Iqbal, Umar
;
Noureldin, Aboelmagd
论文数: 0引用数: 0
h-index: 0
机构:
Queens Univ, Dept Elect & Comp Engn, NavINST Nav & Instrumentat Res Grp, Kingston, ON, Canada
Royal Mil Coll Canada, Dept Elect & Comp Engn, NavINST Nav & Instrumentat Res Grp, Kingston, ON, CanadaTrusted Positioning Inc, Calgary, AB, Canada