In this chapter, the measurement equations of gyroscope and accelerometer and the differential equations of strapdown inertial navigation system (SINS) are presented at first. For high accurate application, in order to reduce the influence of output noise on the calculation accuracy of the system and make full use of the output information, the outputs of gyroscope and accelerometer are all increments, namely the angle increment output by gyroscope and the velocity increment output by accelerometer.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Inertial Autonomous Navigation Technology


    Additional title:

    sp.


    Contributors:
    Wang, Dayi (author) / Li, Maodeng (author) / Huang, Xiangyu (author) / Zhang, Xiaowen (author)


    Publication date :

    2020-08-01


    Size :

    13 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English





    Strapdown inertial navigation technology

    Titterton, David H. ;Weston, John L. | SLUB | 1997


    Strapdown inertial navigation technology

    Titterton, David H. ;Weston, John L. | SLUB | 2004


    Strapdown Inertial Navigation Technology

    Titterton, David H. | TIBKAT | 2004


    Pedestrian Autonomous Positioning System Based on Inertial Navigation

    Xing, Bowen / Jia, Haonan / Liu, Pengfei et al. | British Library Conference Proceedings | 2020