Missile has the advantages of fast speed and strong penetration ability. It has become the main way of high precision strike in modern battleground. The vibration of the missile engine will affect its safety and stability during the active flight. In this paper, Reduced multibody transfer matrix method is used to introduce engine vibration in the missile model considering thrust, establish a missile dynamics model of the active segment flight, derive the total transfer matrix and total transfer equation, and quickly and accurately calculate the transient response of the active segment flight of a certain type of missile, which provides an effective method for studying the influence of engine vibration on the flight performance of the active segment of the missile.


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    Title :

    Research on Missile Vibration Characteristics Considering Engine Vibration Based on Mstmm


    Additional title:

    Lect.Notes Mechanical Engineering


    Contributors:
    Rui, Xiaoting (editor) / Liu, Caishan (editor) / Pu, Yiwen (author) / Gu, Lilin (author) / Wang, Guoping (author) / Liu, Zhengquan (author) / Tang, Jinxin (author)

    Conference:

    International Conference on Mechanical System Dynamics ; 2023 ; Beijing, China September 01, 2023 - September 05, 2023



    Publication date :

    2024-06-18


    Size :

    13 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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