Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Boost and Ascent Trajectory Design and Guidance Approach for Rocket Launched Supersonic Aircraft


    Contributors:
    Liu, Jianhui (author) / Wang, Lansong (author) / Zhang, Mingang (author) / Qin, Xiaoli (author) / Ge, Yajie (author)

    Conference:

    Chinese intelligent systems conference



    Publication date :

    2020-01-01


    Size :

    9 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English



    Optimizing an Ascent Trajectory of a Small Spacecraft Launched by an Air-based Two-Stage Rocket

    Ishkov, Sergey / Balakin, Victor / Khramov, Andrew et al. | IEEE | 2019


    Design of ReFEx Guidance: Trajectory Correction After Ascent

    Gutierrez, Jose Luis R. Redondo / Seelbinder, David / Theil, Stephan | TIBKAT | 2023


    Design of ReFEx Guidance: Trajectory Correction after Ascent

    Redondo Gutierrez, Jose Luis R. / Seelbinder, David / Theil, Stephan | AIAA | 2023



    Aerothermal–Structural Analysis of a Rocket-Launched Mach 8 Scramjet Experiment: Ascent

    Capra, Bianca R. / Brown, L. M. / Boyce, R. R. et al. | AIAA | 2015