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311.
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有人的地方就会有梦。梦也许是人生命中最为瑰丽的部份。在布拖县补姆湿地旁的一个彝族小村庄里,我发现了梦的存在。因为这梦的存在,我觉得我的心和彝人的心不再遥远,我的心与她们一起为生活对生命尊严的挑战而感到颤抖。 相似文献
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随着人工智能技术的发展,智能航空发动机逐渐成为当今航空领域研究的热点。传统的航空发动机控制对发动机模型的依赖性过强,而基于发动机气热动力学公式的机理建模会引入较大的建模误差,给控制器设计带来困难。对此,提出一种基于强化学习的航空发动机控制虚拟自学习方法,首先利用航空发动机的试验数据通过LSTM 神经网络建立虚拟学习环境,然后采用深度强化学习TD3 算法,在虚拟环境中训练智能控制器,最后采用JT9D 发动机模型验证智能控制器的性能。结果表明:相比于传统PID 控制,智能控制器产生的超调量更小,调节时间更短。 相似文献
314.
一种非接触光外差轮廓仪 总被引:1,自引:0,他引:1
介绍了一种纳米级非接触超高精度光外差轮廓仪。该量仪是基于普通光路的外差干涉仪,两束具有微小频差的激光束照射到制件表面:其中一束光被会聚后作为测量光针扫瞄制件表面;另一束光则被用作参考光束。这两束光经反射后形成干涉,所得信号的光程差与制件表面高度变化成正比。量仪的横向分辩力小于2μm,垂直分辩力小于1nm。制件不需要进行大的调整。制件表面同时亦被作为测量参考面。经光电转换后,信号由微机处理,从而快速完成测量、计算、显示与打印各种参数与图形。 相似文献
315.
Dynamicloadisoneoftheimportantoriginalparametersinstructuraldynamicanalysis.Ithasobviousinfluencestodynamicsdesign,vibrationcontrols,activecontroltechnologyandsoon.Sincel97O,manyresearchitemsinthisfieldhavebeenaccomplishedintheworld-Sometheoriesandexperimentalmethodsofdynamicloadidentificationhadbeencreatedinfrequencydomain[l'2J-Howeverftherearesomedisadvantagesthattheycouldbeadaptedonlytoidenti-fythesteady-stateloadandnottoidentifythetransientload,suchasshockloadwithshortsampling.Forvarious… 相似文献
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Honglei Ma Feng Zhang Yu Zhu Yanhua Xiao Abrar Wazir 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
The purpose of the present study was to analyze and predict the changes in acceleration tolerance of human vertebra as a result of bone loss caused by long-term space flight. A human L3–L4 vertebra FEM model was constructed, in which the cancellous bone was separated, and surrounding ligaments were also taken into account. The simulation results demonstrated that bone loss has more of an effect on the acceleration tolerance in x-direction. The results serve to aid in the creation of new acceleration tolerance standards, ensuring astronauts return home safely after long-term space flight. This study shows that more attention should be focused on the bone degradation of crew members and to create new protective designs for space capsules in the future. 相似文献
318.
Yue Wang Shijie Xu Mengping Zhu 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
The full dynamics of spacecraft around an asteroid, in which the spacecraft is considered as a rigid body and the gravitational orbit–attitude coupling is taken into account, is of great value and interest in the precise theories of the motion. The spectral stability of the classical relative equilibria of the full spacecraft dynamics around an asteroid is studied with the method of geometric mechanics. The stability conditions are given explicitly based on the characteristic equation of the linear system matrix. It is found that the linearized system decouples into two entirely independent subsystems, which correspond to the motions within and outside the equatorial plane of the asteroid respectively. The system parameters are divided into three groups that describe the traditional stationary orbit stability, the significance of the orbit–attitude coupling and the mass distribution of the spacecraft respectively. The spectral stability of the relative equilibria is investigated numerically with respect to the three groups of system parameters. The relations between the full spacecraft dynamics and the traditional spacecraft dynamics, as well as the effect of the orbit–attitude coupling, are assessed. We find that when the orbit–attitude coupling is strong, the mass distribution of the spacecraft dominates the stability of the relative equilibria; whereas when the orbit–attitude coupling is weak, both the mass distribution and the traditional stationary orbit stability have significant effects on the stability. We also give a criterion to determine whether the orbit–attitude coupling needs to be considered. 相似文献
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320.
When a wave shaper is embedded in a liner,Mach wave will emerge above the liner,which affects the head shape of an explosively formed projectile.Mach wave parameters,including radius and pressure need to be determined to effectively match Mach wave with the liner,so that a good head shape can be obtained.An analytical calculation model for Mach wave parameter is presented based on three-shock theory,and the theoretical values agree well with the experimental ones.The analysis shows that when the radius of the wave shaper is constant,the radius of the Mach wave increases,whereas the pressure decreases while increasing the distance between the liner and the wave shaper.When the distance between the liner and the wave shaper is constant,the radius of the Mach wave increases,whereas the pressure decreases when decreasing the radius of the wave shaper. 相似文献