| 离箱扰动和折叠翼展开数学模型研究 |
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| 引用本文： | 梁均一.离箱扰动和折叠翼展开数学模型研究[J].上海航天,1997,14(4):3-9. |
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| 作者姓名： | 梁均一 |
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| 作者单位： | 航天工业总公司八院八部 |
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| 摘 要： | 根据箱式发射导轨与导弹，导弹与折叠翼的约束特点，应用动力学普遍定理和解除约束原理，创建了离箱扰动运动数学模型和拆卸叠翼展开过程计算数学模型，并将计算结果与飞行试验结果作了比较。
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| 关 键 词： | 离箱扰动 箱式发射 折叠翼 地空导弹 |
STUDY ON MATHEMATICAL MODELS FOR LEAVING BOX PERTURBATION MOTION AND DEPLOYMENT OF FOLDING WING |
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| Liang Junyi.STUDY ON MATHEMATICAL MODELS FOR LEAVING BOX PERTURBATION MOTION AND DEPLOYMENT OF FOLDING WING[J].Aerospace Shanghai,1997,14(4):3-9. |
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| Authors: | Liang Junyi |
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| Abstract: | This study establishes a mathematical model for missile's leaving box perturbation motion and a mathematical model for the computation of deployment process of folding wing using dynamic common theorem and restraint relieving concept according to restraint properties of box launching guide, missise and folding wing, and compares the results of computation with that of flight test. |
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| Keywords: | Leaving box perturbation Box launching Folding wing Mathematical model Restraint equation |
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