An information combination of star sensor-based angle measurement and inertial devices is used to improve the accuracy of the autonomous navigation system. The missile-borne environment has high dynamic movement characteristics, and the attitude change will bring the star sensor image movement which affects the angular accuracy of the star sensor, thereby reducing navigation accuracy. This paper studies the effect of the attitude of the carrier on the angular measurement of the star sensor, and proposes the accuracy compensation method based on the angular acceleration measurement, thereby improving the angular accuracy of highly dynamics missile-borne star sensors.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Compensation Method of Dynamic Angle Measurement for Missile-Borne Star Sensor


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Yan, Liang (editor) / Duan, Haibin (editor) / Yu, Xiang (editor) / Wu, Bin (author) / Guo, ZhenXi (author) / Ji, Denggao (author) / Chen, Fang (author) / Liu, Quanjun (author)


    Publication date :

    2021-10-30


    Size :

    10 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




    Compensation Method of Dynamic Angle Measurement for Missile-Borne Star Sensor

    Wu, Bin / Guo, ZhenXi / Ji, Denggao et al. | TIBKAT | 2022


    Modular missile borne computers

    Ramseyer, R. / Arnold, R. / Applewhite, H. et al. | NTRS | 1980


    Missile-borne traveling-wave tube

    Apgar, W.D. / Bradford, C.E. | Engineering Index Backfile | 1963


    Missile-borne coaxial unmanned aerial vehicle

    CHEN ZHI / LIN XIANGYU | European Patent Office | 2024

    Free access