An integrated inertial stellar attitude sensor for an aerospace vehicle includes a star camera system, a gyroscope system, a controller system for synchronously integrating an output of said star camera system and an output of said gyroscope system into a stream of data, and a flight computer responsive to said stream of data for determining from the star camera system output and the gyroscope system output the attitude of the aerospace vehicle.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Integrated Inertial Stellar Attitude Sensor


    Contributors:

    Publication date :

    2003


    Size :

    36 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Integrated inertial stellar attitude sensor

    Brady, Tye M. / Kourepenis, Anthony S. / Wyman, Jr., William F. | NTRS | 2007


    Performance Evaluation of a Stellar-Inertial Attitude Sensor Based on Particle Filtering

    Piro, Caterina / Accardo, Domenico / Grassi, Michele | AIAA | 2007


    Performance Evaluation of a Stellar-Inertial Attitude Sensor Based on Particle Filtering AIAA Paper

    Piro, C. / Accardo, D. / Grassi, M. | British Library Conference Proceedings | 2007



    A method of stellar-inertial attitude determination under high dynamic condition

    Li, Han / Lijun, Zhang / Hong, Cai et al. | British Library Online Contents | 2014