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    Title :

    Design of Lateral Control System for a Hypersonic Cruise Missile (AIAA 2017-2111)


    Contributors:
    Fan, Yonghua (author) / Wu, Xiaofei (author) / Xu, Hongyang (author) / Wang, Fan (author)

    Conference:

    AIAA Interantional Space Planes and Hypersonic Systems and Technologies (Conference)



    Publication date :

    2017-01-01


    Size :

    10 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English



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    Design of Lateral Control System for a Hypersonic Cruise missile

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    Heat-augmented Trajectory Optimization of Hypersonic Cruise Vehicle (AIAA 2017-2156)

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    Four-Loop Feedback Control System with Integrator Design for Hypersonic Cruise Missile

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    Nr. 2111

    DataCite | 1886