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靶弹任务规划与虚拟训练技术研究
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作者 曹立飞 曹红松 +3 位作者 刘鹏飞 张芝源 李金新 李超 《测试技术学报》 2021年第3期205-210,共6页
随着军事智能化发展速度的加快,传统的作战训练急需采用智能化技术进行任务规划以及虚拟作战仿真.本文基于便携式安卓设备,开发了高速靶弹供靶任务规划软件,采用JNI技术实现了弹道和射表快速解算,通过OSMDroid实现了供靶点、落点及发射... 随着军事智能化发展速度的加快,传统的作战训练急需采用智能化技术进行任务规划以及虚拟作战仿真.本文基于便携式安卓设备,开发了高速靶弹供靶任务规划软件,采用JNI技术实现了弹道和射表快速解算,通过OSMDroid实现了供靶点、落点及发射方位等参数的图形化显示,基于VR-Forces构建了具有良好视觉沉浸感和交互性的靶弹虚拟仿真系统,用于任务规划结果的仿真与评估.使用结果表明:该系统可以方便高效地完成任务规划及仿真,提高了靶弹训练效率. 展开更多
关键词 高速靶弹 安卓平台 任务规划 训练虚拟仿真
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对厚水层及多层间隙金属靶平面斜侵彻全物理过程的数值模拟研究 被引量:2
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作者 范中波 李恩征 +1 位作者 张凤国 韩冰 《爆炸与冲击》 EI CAS CSCD 北大核心 2002年第1期30-34,共5页
2D平面斜侵彻的数值模拟 ,可再现对应的 3D斜侵彻中最严重非对称受力面内的终点弹道效应 ,并为近似估算 3D斜侵彻等效弹迹及等效扩孔横截面积提供基础数据。利用重新设计和改造的LTZ 2D程序 ,解决了阻抗差异大的多物质厚靶的平面斜侵彻... 2D平面斜侵彻的数值模拟 ,可再现对应的 3D斜侵彻中最严重非对称受力面内的终点弹道效应 ,并为近似估算 3D斜侵彻等效弹迹及等效扩孔横截面积提供基础数据。利用重新设计和改造的LTZ 2D程序 ,解决了阻抗差异大的多物质厚靶的平面斜侵彻的计算问题 ,得到了定性上合理、定量上适用的结果。 展开更多
关键词 多层 阻抗 数值模拟 厚水层 全物理过程 终点道效应 LTZ-2D程序 2D平面斜侵彻 高速碰撞 三角形有限元法
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Acceleration Measurement of Projectile High Velocity Penetrating Concrete Target and Acceleration Signal Analysis 被引量:1
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作者 徐鹏 祖静 范锦彪 《Journal of Measurement Science and Instrumentation》 CAS 2010年第1期22-27,共6页
A kind of novel on-board memory acceleration measure equipment, self-developed, had been employed in recent field test to obtain the acceleration of projectile penetrating many kinds of concrete target. At the same ti... A kind of novel on-board memory acceleration measure equipment, self-developed, had been employed in recent field test to obtain the acceleration of projectile penetrating many kinds of concrete target. At the same time, the aluminintan foam with different density and pore-diameters had been utilized to protect circuit moduies. Furthennore, with the theoretical analysis, computer simulation and field test, the high frequency's impact on the tested acceleration of the projectile had been discussed; At last, the analysis on output signal tested the validity of test data. 展开更多
关键词 acceleration test PROJECTILE penetrate BUFFER
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Discussion of the target-missile control scheme with supersonic speed at minimum altitude
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作者 史震 于秀萍 赵万生 《Journal of Harbin Institute of Technology(New Series)》 EI CAS 2006年第1期16-19,共4页
An antiship missile with supersonic speed at minimum altitude is an effective weapon to break through a defense line. The former Soviet Union was a leader in this field since it had developed several kinds of antiship... An antiship missile with supersonic speed at minimum altitude is an effective weapon to break through a defense line. The former Soviet Union was a leader in this field since it had developed several kinds of antiship missiles which obtained supersonic speed at minimum altitudes. To counter this kind of missile, many countries have been developing corresponding antimissiles. For the purpose of verifing the antimissile missile′s effectiveness in intercepting antiship missiles, a target-missile is needed. A target-missle is cheaper and can imitate the main characteristics of antiship missiles with supersonic speed at minimum altitude. In this paper, the control scheme of a target missile flying with supersonic speed at minimum altitude is studied. To counter the problem of hedgehopping over the sea, a control scheme utilizing a SINS+altimeter was proposed. In this scheme, both the quick response ability of altitude control and the anti-jamming problem were considered. A simulation experiment shows that when an integrated altitude control system is used, the anti-disturbance ability of the integrated altitude is good and the response speed of altitude control system can be dramatically improved. 展开更多
关键词 SUPERSONIC minimum altitude target missile integrated altitude
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