航空发动机虚拟自学习控制方法研究

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。     

天基信息支援对导弹攻防作战的效用分析

分析了空天一体作战天基装备系统——军事卫星,对导弹攻防作战重要的信息支援效用。建立并阐述了天基军事卫星信息系统信息支援下导弹攻防作战过程模型和影响图模型,对模型进行了详细的分析讨论。     

机床主轴加工工艺教学案例分析——以CA6140车床主轴机械加工为例

针对<机械制造工艺基础>课程中实验内容较少的实际情况,在教学过程中,应该提倡增加实践教学环节,提高学生的实际动手能力,本文以CA6140机床主轴加工工艺为例,详细说明加工路线的制定、定位基准的选择及CA6140机床主轴的加工工艺过程的制定,使学生熟悉制订工艺过程的原则,步骤和方法,培养合理确定工艺过程的技能.     

我国静脉产业发展的投融资问题与对策探讨

发展静脉产业对于改造或调控现行物质流模式，提高资源和能源的利用效率，形成资源和能源的高效物质循环模式具有重要意义。本文基于我国静脉产业的发展现状，针对静脉产业发展的投融资问题进行了分析，提出了相应的对策和模式建议，为我国静脉产业发展在投融资方面提供了一定的借鉴。     

Comparative analysis of chemical composition and optical properties of gaseous and disperse phases of the Earth-group planetary atmospheres

The models of chemical composition and structure of the Earth-type planetary atmospheres are offered. The optical properties of gaseous and disperse phases of the atmospheres are investigated.     

Initial results from COMPTEL onboard GRO

COMPTEL is the first imaging telescope to explore the MeV gamma-ray range (0.7 to 30 MeV). At present, it is performing a complete sky survey. In later phases of the mission selected celestial objects will be studied in more detail. The data from the first year of the mission have demonstrated that COMPTEL performs very well. First sky maps of the inner part of the Galaxy clearly identify the plane as a bright MeV-source (probably due to discrete sources as well as diffuse radiation). The Crab and Vela pulsar lightcurves have been measured with unprecedented accuracy. The quasars 3C273 and 3C279 have been seen for the first time at MeV energies. Both quasars show a break in their energy spectra in the COMPTEL energy range. The 1.8 MeV line from radioactive ²⁶A1 has been detected from the central region of the Galaxy and a first sky map of the inner part of the Galaxy has been obtained in the light of this line. Upper limits to gamma-ray line emission at 847 keV and 1.238 MeV from SN 1991T have been derived. Upper limits to the interstellar gamma-ray emissivity have been determined at MeV-energies. Several cosmic gamma-ray bursts within the field-of-view have been located with an accuracy of about 1°. On 1991 June 9, 11 and 15, COMPTEL observed gamma-ray emission (continuum and line) from three solar flares. Also neutrons were detected from the June 9 and June 15 flares.     

Pulsar studies with GRO-COMPTEL

Pulsar measurements performed by the experiment COMPTEL, aboard the Compton Gamma Ray Observatory, are described. The main results refer to the Crab and Vela pulsars whose pulse shape characteristics are given in some detail and light curves are compared with those above 50 MeV, as observed by the COS-B satellite. No other gamma-ray pulsars have been detected to date by COMPTEL, the upper limit on the pulsed signal from Geminga being compatible with indications by other experiments.     

The gravity-darkening of the main-sequence components of spectral types A, F and G in detached close binary systems

From analysis of the photometric ellipticity effect in seven well-understood detached close binary systems, empirical values of the exponent of gravity-darkening have been practically deduced for eleven main-sequence components of spectral types A, F and G which should cover the range of structural change (from radiative to convective) in stellar atmospheres. The result indicate that values of the exponent diminish gradually with decreasing effective temperatures from 1.0 for radiative atmospheres with T > 8500 K to = 0.2 0.3 for convective atmospheres with T < 6500 K, in spite of some uncertainty in the reflection correction process.     

一种非接触光外差轮廓仪

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。     

固体火箭发动机／导弹一体化设计

以某一两级固体地—空导弹作为算例,研究了固体火箭发动机/导弹一体化设计问题。研究以导弹起飞质量最轻和可用过载最大为目标建立了目标函数,利用优化理论完成了7个设计变量的优化设计。优化结果表明,所建立的数学模型是正确的。