Tightly Coupled Modeling and Reliable Fusion Strategy for Polarization-Based Attitude and Heading Reference System

被引:29
作者
Liu, Xin [1 ]
Yang, Jian [1 ,2 ]
Li, Wenshuo [2 ]
Huang, Panpan [2 ]
Guo, Lei [1 ,2 ]
机构
[1] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China
[2] Beihang Univ, Hangzhou Innovat Inst, Hangzhou 310051, Peoples R China
基金
中国国家自然科学基金; 国家重点研发计划;
关键词
Reliability; Mathematical models; Accelerometers; Measurement uncertainty; Gyroscopes; Global navigation satellite system; Compass; Partial loss or occlusion of the optical signal; polarization-based attitude and heading reference system (PAHRS); polarization-based tightly coupled model (PTCM); polarized skylight intensity; reliable fusion strategy; KALMAN FILTER; OBSERVABILITY ANALYSIS; INERTIAL NAVIGATION;
D O I
10.1109/TII.2022.3160164
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
The polarization-based attitude and heading reference system (PAHRS) provides an effective solution for attitude and heading information acquisition. Its practical performance, however, will be degraded due to partial loss and/or occlusion of the optical signal. To improve the adaptivity of PAHRS, in this article, we establish a polarization-based tightly coupled model (PTCM) and propose a reliable fusion strategy for information extraction from the polarization sensor (PS) and inertial navigation system (INS). As compared to the existing PS/INS fusion model, the proposed PTCM directly adopt PS raw observations (polarized skylight intensity) to compensate for the accumulation errors of INS, thereby removing the constraints on the least number of PS observation channels and avoiding nonlinear transformation of PS noises. Moreover, the reliable fusion strategy consists of a reliable observation channel selection step followed by a nonlinear filtering step, which can reduce the effect of unreliable polarized skylight intensity measurement. Finally, the simulation, static and semi-physical vehicle-mounted tests confirm the effectiveness of the proposed PTCM and fusion strategy.
引用
收藏
页码:62 / 73
页数:12
相关论文
共 25 条
[1]  
Aycock T.M., 2018, US Patent, Patent No. [9,989,625, 9989625]
[2]   Multimodal Sensor Fusion for Attitude Estimation of Micromechanical Flying Insects: a Geometric Approach [J].
Campolo, Domenico ;
Schenato, Luca ;
Pi, Lijuan ;
Deng, Xinyan ;
Guglielmelli, Eugenio .
2008 IEEE/RSJ INTERNATIONAL CONFERENCE ON ROBOTS AND INTELLIGENT SYSTEMS, VOLS 1-3, CONFERENCE PROCEEDINGS, 2008, :3859-+
[3]   Attitude Estimation of a Biologically Inspired Robotic Housefly via Multimodal Sensor Fusion [J].
Campolo, Domenico ;
Schenato, Luca ;
Pi, Lijuan ;
Deng, Xinyan ;
Guglielmelli, Eugenio .
ADVANCED ROBOTICS, 2009, 23 (7-8) :955-977
[4]   IM-Filter for INS/GPS-Integrated Navigation System Containing Low-Cost Gyros [J].
Cho, Seong Yun .
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2014, 50 (04) :2619-2629
[5]   An Autonomous Initial Alignment and Observability Analysis for SINS With Bio-Inspired Polarized Skylight Sensors [J].
Du, Tao ;
Tian, Changzheng ;
Yang, Jian ;
Wang, Shanpeng ;
Liu, Xin ;
Guo, Lei .
IEEE SENSORS JOURNAL, 2020, 20 (14) :7941-7956
[6]   AntBot: A six-legged walking robot able to home like desert ants in outdoor environments [J].
Dupeyroux, Julien ;
Serres, Julien R. ;
Viollet, Stephane .
SCIENCE ROBOTICS, 2019, 4 (27)
[7]   UAV Attitude Estimation Using Unscented Kalman Filter and TRIAD [J].
Garcia de Marina, Hector ;
Pereda, Fernando J. ;
Giron-Sierra, Jose M. ;
Espinosa, Felipe .
IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2012, 59 (11) :4465-4474
[8]   A Novel Method to Integrate IMU and Magnetometers in Attitude and Heading Reference Systems [J].
Han, Songlai ;
Wang, Jinling .
JOURNAL OF NAVIGATION, 2011, 64 (04) :727-738
[9]   A Combination Orientation Compass Based on the Information of Polarized Skylight/Geomagnetic/MIMU [J].
He, Ruiguang ;
Hu, Xiaoping ;
Zhang, Lilian ;
He, Xiaofeng ;
Han, Guoliang .
IEEE ACCESS, 2020, 8 :10879-10887
[10]   Correlation-Averaging Methods and Kalman Filter Based Parameter Identification for a Rotational Inertial Navigation System [J].
Hu, Peida ;
Chen, Bingxu ;
Zhang, Chenxi ;
Wu, Qiuping .
IEEE TRANSACTIONS ON INDUSTRIAL INFORMATICS, 2019, 15 (03) :1321-1328