This paper presents a guidance method for solid-rocket launch vehicles. A three-stage launch vehicle, as illustration, the guidance algorithm is designed for the second stage and the third stage. For the second stage, the guidance algorithm guides the vehicle to a transfer orbit, and high precision orbit injection is implemented by the guidance algorithm for the third stage. Numerical simulation results show that the proposed guidance method can achieve an adequate precision with the burnout shutdown.


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    Title :

    A Guidance Method for Small Solid-Rocket Launch Vehicles


    Contributors:
    Lv, Rui (author) / Song, Zhiguo (author) / Li, Pu (author) / Jiang, Chunwang (author) / Ge, Yunpeng (author)


    Publication date :

    2018-08-01


    Size :

    111331 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English







    An Energy Management Ascent Guidance Algorithm for Solid Rocket-Powered Launch Vehicles

    Xu, H. / Chen, W. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011