Adaptive BDS/MEMS INS navigation algorithm for low-dynamic carrier based on motion characteristics detection and dual-antenna Position/ Velocity constraints

被引:2
作者
Feng, Yihang [1 ,4 ]
Huang, Guanwen [1 ,2 ]
Li, Xin [1 ,2 ]
Li, Zhenhong [1 ,3 ,4 ]
Jing, Ce [1 ,4 ]
Zhang, Kai [1 ,4 ]
机构
[1] Changan Univ, Coll Geol Engn & Geomat, Xian 710054, Peoples R China
[2] Minist Nat Resources, Key Lab Ecol Geol & Disaster Prevent, Xian 710054, Peoples R China
[3] Minist Educ, Key Lab Western Chinas Mineral Resource & Geol Eng, Xian 710054, Peoples R China
[4] Changan Univ, Big Data Ctr Geosci & Satellites, Xian 710054, Peoples R China
基金
中国国家自然科学基金;
关键词
BDS; MEMS INS; Low-dynamic carrier motion characteristics; Dual-antenna constraint information; ACCURACY;
D O I
10.1016/j.measurement.2023.114037
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
With the rapid development of navigation technology, the application fields of unmanned technology are expanding constantly, including the low-dynamic scenarios, such as unmanned agricultural machinery. In a low-dynamics scenario, the classic dual-antenna BeiDou Navigation Satellite System (BDS)/micro-electro-mechanical system inertial navigation system (MEMS INS) integrated navigation algorithm has two limitations. First, the reliability of a priori system noise is significantly reduced because of the large number of turning and bumping maneuvers. Second, the accuracy of the dual-antenna BDS heading angle and a priori measurement noise cannot satisfy the necessary requirements in a complex environment. To solve these problems, an adaptive BDS/MEMS INS navigation algorithm based on low-dynamic carrier-motion characteristics and dual-antenna constraint in-formation is proposed. This new method can identify turning and bumping states and appropriately adjust the MEMS INS system noise matrix. To avoid the influence of a low accuracy heading angle, the heading angle measurement information was replaced by position and velocity measurement information. Simultaneously, the velocity and distance vectors between the dual antennas are added as prior constraints that can adaptively adjust the BDS measurement noise matrix. The experimental results show that the positioning and heading angle ac-curacies of the proposed method are controlled within centimeters and 1 degrees, respectively, thus significantly improving the navigation performance in the carrier turning, bumping, and occlusion environments. This research will be helpful in low-dynamic applications such as unmanned agricultural machinery.
引用
收藏
页数:10
相关论文
共 36 条
[1]   Land-vehicle navigation using GPS [J].
Abbott, E ;
Powell, D .
PROCEEDINGS OF THE IEEE, 1999, 87 (01) :145-162
[2]   Integrity of an integrated GPS/INS system in the presence of slowly growing errors. Part I: A critical review [J].
Bhatti, Umar I. ;
Ochieng, Washington Y. ;
Feng, Shaojun .
GPS SOLUTIONS, 2007, 11 (03) :173-181
[3]   Sensors key to advances in precision agriculture [J].
Bogue, Robert .
SENSOR REVIEW, 2017, 37 (01) :1-6
[4]   Centimetre-precision guidance of moving implements in the open field: a simulation based on GPS measurements [J].
Dijksterhuis, HL ;
Van Willigenburg, LG ;
Van Zuydam, RP .
COMPUTERS AND ELECTRONICS IN AGRICULTURE, 1998, 20 (03) :185-197
[5]   Inertial sensors technologies for navigation applications: state of the art and future trends [J].
El-Sheimy, Naser ;
Youssef, Ahmed .
SATELLITE NAVIGATION, 2020, 1 (01)
[6]   Implement lateral position accuracy under RTK-GPS tractor guidance [J].
Gan-Mor, Samuel ;
Clark, Rex L. ;
Upchurch, Bruce L. .
COMPUTERS AND ELECTRONICS IN AGRICULTURE, 2007, 59 (1-2) :31-38
[7]   An integrated land vehicle navigation system based on context awareness [J].
Gao, Nan ;
Zhao, Long .
GPS SOLUTIONS, 2016, 20 (03) :509-524
[8]   Assessing the accuracy of NRTK altimetric positioning for precision agriculture: test results in an olive grove environment in Southeast Spain [J].
Garrido, M. S. ;
de Lacy, M. C. ;
Ramos, M. I. ;
Borque, M. J. ;
Susi, M. .
PRECISION AGRICULTURE, 2019, 20 (03) :461-476
[9]  
Ge B.S., 2020, Navigation Positioning Timing, V7, P48
[10]  
Groves P.D, 2015, IEEE AERO EL SYS MAG, V30, P26, DOI 10.1109/MAES.2014.14110