Launch Dynamics Modeling and Analysis on Influencing Factors for Airborne Missile

LIAO  Shasha; WU  Cheng; DUAN  Ji

doi:10.15892/j.cnki.djzdxb.2013.03.049

Journal of Projectiles, Rockets, Missiles and Guidance >

2013 , Vol. 33 >Issue 3: 153 - 156,162

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2013.03.049

CORRELATION TECHNOLOGY

Launch Dynamics Modeling and Analysis on Influencing Factors for Airborne Missile

LIAO Shasha ,
WU Cheng ,
DUAN Ji

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State Key Laboratory of Explosion Science and Technology, Beijing Institute of Technology, Beijing 100081, China

Received date: 2012-08-28

Online published: 2025-05-26

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Abstract

According to the characteristics of oriented-rail launch technique for airborne missile, launch dynamics and kinematics models were established. Some influence factors were analyzed, including pneumatic force, launch obliquity, slide length, thrust misalignment and stochastic wind disturbance. Based on simulation and calculation for airborne missile launch system, movement parameters and laws of the missile away slide were obtained. The simulation conclusion accords with practices, providing theory basis for oriented-rail launch system design.

Key words： airborne missile; launch dynamics; thrust misalignment; wind disturbance model

Cite this article

LIAO Shasha , WU Cheng , DUAN Ji . Launch Dynamics Modeling and Analysis on Influencing Factors for Airborne Missile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2013 , 33(3) : 153 -156,162 . DOI: 10.15892/j.cnki.djzdxb.2013.03.049

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