A rapid and accurate transfer alignment method using inertial instrument measurement information

被引:0
|
作者
Li, Zhaoqi [1 ]
Wang, Xinlong [1 ]
Ding, Wei [2 ]
Nie, Guanghao [2 ]
机构
[1] Beihang Univ, Sch Astronaut, Beijing 100083, Peoples R China
[2] Beijing Inst Control & Elect Technol, Beijing 100038, Peoples R China
关键词
Transfer alignment; Flexural deformation; Relative attitude estimation; Angular increment matching quantity; Specific force matching quantity; FILTER;
D O I
10.1016/j.measurement.2024.116112
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The rapidity and precision of transfer alignment impacts the response speed and working precision of inertial navigation system (INS) directly, and flexural deformation is a critical constraint on transfer alignment performance. However, transfer alignment performance of the traditional modeling estimation method is easily degraded by the effect of model mismatch. Therefore, a rapid and accurate transfer alignment method using inertial instrument measurements is proposed in this paper. The relative attitude of main/sub INSs is roughly estimated by angular velocity measurements. Then, a novel transfer alignment filter model is established by relative attitude error model, and measurements of inertial instrument are used to construct angular increment matching and specific force matching quantities. This approach improves both the rapidity and precision of sub INS's alignment. The performance validation results indicate that compared with traditional methods, the proposed method can improve alignment accuracy by more than 70% and significantly shorten alignment time, thus realizing rapid and accurate alignment.
引用
收藏
页数:13
相关论文
共 50 条
  • [1] The transfer alignment method based on the inertial network
    Chen, Weina
    Yang, Zhong
    Gu, Shanshan
    Tang, Yujuan
    Wang, Yizhi
    OPTIK, 2020, 217
  • [2] Observability and alignment error analysis for rapid transfer alignment of inertial navigation system
    Coll. of Automation, Harbin Engineering Univ., Harbin 150001, China
    Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics, 2007, 29 (12): : 2111 - 2116
  • [3] Rapid transfer alignment of an inertial navigation system using a marginal stochastic integration filter
    Zhou, Dapeng
    Guo, Lei
    MEASUREMENT SCIENCE AND TECHNOLOGY, 2018, 29 (01)
  • [4] Optimisation-based Transfer Alignment and Calibration Method for Inertial Measurement Vector Integration Matching
    Xie, Lili
    Lu, Jiazhen
    JOURNAL OF NAVIGATION, 2017, 70 (03): : 595 - 606
  • [5] NEW INSTRUMENT FOR RAPID AND ACCURATE MEASUREMENT OF ULTRASONIC VELOCITY AND ATTENUATION USING A MINICOMPUTER SYSTEM
    NAKAJIMA, H
    TANAKA, H
    SHIMAZAKI, O
    YAMANAKA, K
    KINOSHITA, T
    WADA, Y
    JAPANESE JOURNAL OF APPLIED PHYSICS, 1979, 18 (07) : 1379 - 1385
  • [6] Observability and maneuvering for rapid transfer alignment of a strapdown inertial navigation system
    Kong, Xingwei
    Guo, Meifeng
    Dong, Jingxin
    Qinghua Daxue Xuebao/Journal of Tsinghua University, 2010, 50 (02): : 232 - 236
  • [7] Rapid transfer alignment of laser SINS using quaternion based angular measurement
    Dai, Hongde
    Dai, Shaowu
    Cong, Yuancai
    Zhao, Guorong
    Wu, Guangbin
    OPTIK, 2013, 124 (20): : 4364 - 4368
  • [8] A method for rapid transfer alignment based on UKF
    Wang Ya-Feng
    Sun Fu-chun
    Zhang You-an
    2006 IMACS: MULTICONFERENCE ON COMPUTATIONAL ENGINEERING IN SYSTEMS APPLICATIONS, VOLS 1 AND 2, 2006, : 809 - +
  • [9] Research of Transfer Alignment for Airborne Distributed Inertial Attitude Measurement System
    Wang, Yukun
    Chen, Shuai
    Li, Xian
    Zhong, Runwu
    PROCEEDINGS OF THE 3RD INTERNATIONAL CONFERENCE ON ELECTRIC AND ELECTRONICS, 2013, : 261 - 264
  • [10] Rapid and Accurate INS Transfer Alignment for Air Launched Tactical Missile Using Kalman Filter
    Jain, Sambhav Kumar
    Jain, Tapan K.
    Shanker, Saumya
    Srivastava, Srikant
    DEFENCE SCIENCE JOURNAL, 2023, 73 (04) : 496 - 502