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超空泡航行体非定常流体动力延迟效应水洞试验研究 被引量:3
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作者 刘喜燕 袁绪龙 +2 位作者 王鹰 罗凯 汪新禹 《实验流体力学》 CAS CSCD 北大核心 2021年第5期26-33,共8页
空泡延迟效应在机动航行诱发的尾拍振荡中影响显著,是超空泡航行体的重要力学特性,在动力学建模中必须加以考虑。采用人工通气超空泡的试验方法,在西北工业大学高速水洞实验室开展了超空泡航行体连续变攻角测力试验研究,测量攻角与流体... 空泡延迟效应在机动航行诱发的尾拍振荡中影响显著,是超空泡航行体的重要力学特性,在动力学建模中必须加以考虑。采用人工通气超空泡的试验方法,在西北工业大学高速水洞实验室开展了超空泡航行体连续变攻角测力试验研究,测量攻角与流体动力随时间变化历程来定量分析延迟时间特性。通过试验研究,获得了不同试验条件下变化的延迟时间;无量纲化的延迟系数与水速近似成线性关系,且随预置舵角的增大而增大;在试验采用的摆动频率中,摆动频率较大的工况,延迟系数较小。 展开更多
关键词 超空泡航行 尾拍效应 机动航行 延迟效应 水洞试验
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GUIDANCE AND CONTROL FOR AUTOMATIC LANDING OF UAV 被引量:1
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作者 曹云峰 陶勇 沈勇璋 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2001年第2期229-235,共7页
A scheme of guidance and control is presented to meet the requirements for automatic landing of unmanned aerial vehicles (UAVs) based on the airborne digital flight control system and radio tracker on ground station. ... A scheme of guidance and control is presented to meet the requirements for automatic landing of unmanned aerial vehicles (UAVs) based on the airborne digital flight control system and radio tracker on ground station. An automatic landing system is realized for an unmanned aerial vehicle. The results of real time simulation and flight test are given to illustrate the effectiveness and availability of the scheme. Results meet all the requirements for automatic landing of the unmanned aerial vehicle. 展开更多
关键词 automatic landing unmanned aerial vehicle GUIDANCE NAVIGATION flight control
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以色列Descaver诱饵系统
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作者 乙一 《舰船电子对抗》 1996年第6期37-37,共1页
Deseaver是以色列Elbit有限公司研制的诱饵控制和发射系统。 该系统可完成下述任务:①评估威胁战术态势,并选择合适的无源对抗措施;②与EW防御系统相连工作,与舰艇的整个作战系统相协调;③部署过程计算;④推荐舰艇机动航行以脱离危险区... Deseaver是以色列Elbit有限公司研制的诱饵控制和发射系统。 该系统可完成下述任务:①评估威胁战术态势,并选择合适的无源对抗措施;②与EW防御系统相连工作,与舰艇的整个作战系统相协调;③部署过程计算;④推荐舰艇机动航行以脱离危险区;⑤发射防御诱饵;⑥控制6种EW火箭(箔条和红外);⑦根据所选程序进行资源分配并发射火箭;⑧部署战术诱饵;⑨为指挥官提供威胁和诱饵环境的显示。 展开更多
关键词 诱饵 有效载荷 作战系统 无源对抗 资源分配 辐射强度 机动航行 发射系统 防御系统 留空时间
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A Potential Flow Based Flight Simulator for an Underwater Glider 被引量:3
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作者 Surasak Phoemsapthawee Marc Le Boulluec +1 位作者 Jean-Marc Laurens Fran ois Deniset 《Journal of Marine Science and Application》 2013年第1期112-121,共10页
Underwater gliders are recent innovative types of autonomous underwater vehicles (AUVs) used in ocean exploration and observation. They adjust their buoyancy to dive and to return to the ocean surface. During the ch... Underwater gliders are recent innovative types of autonomous underwater vehicles (AUVs) used in ocean exploration and observation. They adjust their buoyancy to dive and to return to the ocean surface. During the change of altitude, they use the hydrodynamic forces developed by their wings to move forward. Their flights are controlled by changing the position of their centers of gravity and their buoyancy to adjust their trim and heel angles. For better flight control, the understanding of the hydrodynamic behavior and the flight mechanics of the underwater glider is necessary. A 6-DOF motion simulator is coupled with an unsteady potential flow model for this purpose. In some specific cases, the numerical study demonstrates that an inappropriate stabilizer dimension can cause counter-steering behavior. The simulator can be used to improve the automatic flight control. It can also be used for the hydrodynamic design optimization of the devices. 展开更多
关键词 underwater glider potential flow Newton-Euler equation autonomous underwater vehicles (AUVs) flight simulator
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