Effect of injection scheme on asymmetric phenomenon in rectangular and circular scramjets

The asymmetric separation has a crucial effect on the performance of the scramjet. In this study, the asymmetric separation and combustion in both rectangular and circular scramjets are investigated numerically, and the effect of injection scheme is analyzed. The characteristics of the flow field are analyzed based on sufficient code verification. In the rectangular scramjet, the separation tends to occur in the corner due to the corner boundary-layer effect. The separation is asymmetric and only two corners have serious separation. The fuel penetration depth in the separation zone increases and the combustion is intensified. When the injection scheme is uniform, both the combustion and separation become weak. In the circular scramjet, the separation and combustion are basically axisymmetric in the scramjet with one-row injection scheme. The asymmetric combustion becomes obvious in cases with multi-row injection scheme. When the injection orifices distribute intensively on the top and bottom sides, the strongest and weakest separations occur near these two sides respectively. When the distribution of orifices becomes uniform, the direction of separation cannot be predicted. For multi-row cases, the nonuniform injection scheme could result in violent combustion and asymmetric flow structures compared with the uniform injection scheme.     

鲁西黄牛肉用品系核心群育种方案遗传和经济评估

针对鲁西黄牛肉用品系现行的核心群育种方案,以育种最大投资回报率为评估标准,通过活体质量、繁殖、日增质量和胴体性状测定记录作为选择信息,根据使用不同可利用记录作为不同选种的标准设定了4种选择方案(方案1:活体质量信息+日增质量信息;方案2:活体质量信息+繁殖信息;方案3:方案1+方案2;方案4:方案3+胴体性状信息),并采用确定性模型评估了4种选择方案的遗传进展和育种效益.结果表明,4种选择方案的年综合育种进展分别为21.87、34.08、38.09和54.86元;育种效益为147.39、204.44、241.83和309.05元;投入产出比为1∶ 3.78、1∶ 4.60、1∶ 5.14和1∶ 5.77;平均世代间隔均为5.53年.以上数据表明,随着可利用信息在选择标准中的变化,遗传进展和育种效益也随之变化,选择方案4可获得较好的育种效果,所以,在现行育种方案中,采用方案4可获得理想的育种效果.     

Finite time non-singular sliding mode control for spinning tether system with prescribed performance under artificial gravity mission

In this paper, the spinning tether system (STS) is applied to produce the artificial gravity overload with a proposed spin-up scheme in elliptical transfer orbits. To improve the comfort of the astronauts during spinning, the combined control scheme with tension and thrust is designed for spin-up. Then, based on the novel performance function and sliding mode technology, a finite time prescribed performance controller is proposed to track angular velocity for the desired artificial gravity overload. Compared with the existing works, the tracking error is controlled within the preset transient performance and converged to the origin within finite time even in the presence of unknown external disturbance. The stability of closed-loop tracking system is proved by Lyapunov theorem. Finally, the numerical simulations are given to demonstrate the effectiveness and robustness of the proposed controllers in the artificial gravity mission.     

具有欺骗攻击的主从神经网络混合 事件触发同步控制

文章提出了一种针对受到欺骗攻击的主从神经网络的混合事件触发同步控制方法。所提出的方法采用以伯努利分布为特征的混合事件触发方案，通过仅在必要时传输数据来减轻通信负担并处理不可预测的网络环境。记忆事件触发机制可以在系统响应状态的峰值和低谷期间传输更多的数据。通过考虑实际情况中的不确定性，将网络诱导时滞和随机发生的欺骗攻击纳入一个统一的框架，并构建了相应的李雅普诺夫泛函。其次，使用李雅普诺夫理论，推导出一个稳定性判据。最后，通过数值算例验证了所提出方法的有效性。     

基于适航管理和RCM的军用运输机维修管理体系

本文介绍了以可靠性为中心的维修(RCM)管理过程及特点,可靠性方案与维修方案的关系,可靠性方案的组成要素、实现方式以及在维修管理中的作用,分析了军用运输机部队制定以可靠性为中心的维修管理方案的必要性和可行性,并提出了制定方案的方法。     

基于 PDPC-EMV模型的装备研制方案优化设计

将全面质量管理的过程决策程序图法(PDPC)与决策分析技术的期望值法(EMV)有机结合,构建了PDPC-EMV理论模型,并将该模型引入到武器装备研制方案的设计环节中,用风险评估的思维解决全面质量管理的问题,为武器装备研制方案的设计工作开辟了一种先期质量控制思路。