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高超声速飞行器动力滑翔组合弹道优化 被引量:1
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作者 魏继华 王兆魁 《指挥与控制学报》 CSCD 2021年第3期249-256,共8页
将滑翔弹道与巡航弹道的优势结合起来,设计了一种"滑翔+高马赫数巡航"飞行弹道方案,首先以增大射程和纵横向机动能力为指标,基于Gauss伪谱法优化设计了高超声速滑翔弹道方案;然后以反馈线性化结合滑模变结构理论,设计了高精... 将滑翔弹道与巡航弹道的优势结合起来,设计了一种"滑翔+高马赫数巡航"飞行弹道方案,首先以增大射程和纵横向机动能力为指标,基于Gauss伪谱法优化设计了高超声速滑翔弹道方案;然后以反馈线性化结合滑模变结构理论,设计了高精度稳态巡航方案.弹道仿真结果表明,新弹道方案能迅速收敛于最优解,从而验证了所设计弹道的合理性. 展开更多
关键词 高超声速飞行器 滑翔巡航 组合弹道 轨迹优化
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航空时敏制导炸弹增程弹道组合优化设计 被引量:8
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作者 白宏阳 李伟明 +1 位作者 孙瑞胜 熊舒望 《国防科技大学学报》 EI CAS CSCD 北大核心 2014年第6期100-105,共6页
为增强航空时敏制导炸弹在中制导段的滑翔能力,将极小值原理与自适应进化粒子群算法相结合,提出了一种适用于航空时敏制导炸弹增程弹道的组合优化设计方法。基于纵向平面内质心运动模型,推导了性能指标泛函及各不等式约束函数。引入Lagr... 为增强航空时敏制导炸弹在中制导段的滑翔能力,将极小值原理与自适应进化粒子群算法相结合,提出了一种适用于航空时敏制导炸弹增程弹道的组合优化设计方法。基于纵向平面内质心运动模型,推导了性能指标泛函及各不等式约束函数。引入Lagrange乘子矢量并建立相应的Hamilton函数实现无约束泛函极值问题的转换,推导出兼顾各优化目标函数的满意优化模型。利用自适应进化粒子群算法对该段增程弹道进行了攻角与弹翼张合档位双设计变量的组合优化。数值仿真算例表明,在满足状态方程约束的条件下,双变量的增程效果比常规单变量控制时显著提高,其优化结果可为制导炸弹弹道规划设计的研究提供一定的理论参考。 展开更多
关键词 时敏制导炸弹 弹道组合优化 自适应进化粒子群 最优控制
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Mechanical and ballistic properties of powder metal 7039 aluminium alloy joined by friction stir welding 被引量:1
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作者 Mehmet ERDEM Hanifi CINICI +2 位作者 Ugur GOKMEN Halil KARAKOC Mehmet TURKER 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2016年第1期74-84,共11页
7039 Al alloy plates which were used as armor materials were produced by powder metallurgy method. The prepared mixed powders were pressed and plated by extrusion process. These plates, after being subjected to T6 hea... 7039 Al alloy plates which were used as armor materials were produced by powder metallurgy method. The prepared mixed powders were pressed and plated by extrusion process. These plates, after being subjected to T6 heat treatment, were joined double-sided by friction stir welding method. Microstructure and microhardness of the welded plate were investigated. It was determined that the finest grain structure and the lowest hardness value occurred in the stir zone as 2-6 mm and HV 80.9, respectively. In order to determine the ballistic properties of welded plates, 7.62 mm armor piercing projectiles were shot to the base metal(BM), heat affected zone(HAZ), and thermomechanically affected zone+stir zone(TMAZ+SZ). Ballistic limits(v_(50)) of these zones were determined. The ballistic limits of the BM, TMAZ+SZ, and HAZ of the plate were approximately 14.7%, 15.3%, and 17.9% lower than that of the standard plate at the same thickness, respectively. It was determined that the armor piercing projectiles created petaling and ductile hole enlargement failure types at the armor plate. Ballistic and mechanical results can be enhanced by hot-cold rolling mills after extrusion and particle reinforcement. 展开更多
关键词 powder metal 7039 Al alloy ballistic limit microstructure mechanical properties
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