The gyrowheel can be used as an actuator to provide three-axis control torque for spacecraft, and also as a sensor to measure the two-axis attitude angular velocity of spacecraft. The existence of non ideal factors is the key factor affecting the measurement of spacecraft angular velocity with gyrowheel. Therefore, this paper mainly studies the non-ideal factor that the support torsion bar of gyrowheel is not perpendicular and analyzes the non-perpendicularity support on the measurement accuracy of spacecraft attitude angular velocity.


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    Title :

    Analysis of the Perpendicularity Influence of the Gyrowheel Support on the Spacecraft Angular Velocity Measurement Accuracy


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Yan, Liang (editor) / Duan, Haibin (editor) / Yu, Xiang (editor) / Xiaokun, Liu (author) / Jian, Zhang (author) / Jun, Fu (author) / Dongqing, Gu (author) / Bin, Song (author)


    Publication date :

    2021-10-30


    Size :

    7 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English





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