This paper establishes the kinetic model of S&A mechanisms used on missiles flying flexibly on the condition of large lateral acceleration and small axial acceleration through dynamics and kinematics analysises.The model could be universally applied to the research on the safety systems'ability to eliminate lateral acceleration effects on ground-air and air-air missiles.%以一种载体作高机动飞行的远距离解除保险机构为对象,通过动力学和运动学分析,建立了在大横向过载、小轴向过载作用下的系统运动模型。该模型对研究地空和空空导弹用安全系统抗横向过载能力具有一般意义。
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