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1.
随着软件的应用规模越来越大,软件系统一旦出现故障,很可能会造成人员伤亡或财产等重大损失,因此对软件可信性进行评估尤为重要.在安全攸关如航空航天等领域,作为可信关键属性之一的安全性影响着整个软件系统的可信评估.特别当一个组件受到安全攻击或缺陷出现时,可信性会下降,会影响到与它可信关联的组件可信性,从而影响到整个系统的可信性.遵循这一思路,设计了软件系统组件可信性发生改变后对其它组件可信性影响度量公式,进一步给出当一组件可信性发生变化,整个软件系统各组件可信性度量发生变化的度量模型.本文以某“航天电源管理设备”为例,证明了本文所建立的组件可信依赖关系度量模型的合理性和有效性. 相似文献
2.
Yi Wei Qingjun Li Fangnuan Xu 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(1):393-400
A new orbit-attitude-vibration coupled dynamic model of the tethered solar power satellite (Tethered SPS) is established based on absolute nodal coordinate formulation. The Hamilton’s equation of the system is derived by introducing generalized momentum through Legendre transformation. The correctness of the proposed model is verified by an example. The dynamic characteristics of the Tethered SPS are studied using the symplectic Runge-Kutta method. Simulation results show that the orbital radius and the total energy of the system are well preserved. The attitude of the system is unstable when the mass of the bus system is small. However, the attitude stability is dependent on some other parameters of the system, which requires further studies. It is also found that the average tether force/deformation can be roughly estimated by simplifying the solar panel as a particle. The proposed model can be used to study the orbit-attitude-vibration coupled dynamics and control problems. 相似文献
3.
对激光通信终端在轨瞬态温度变化开展了仿真,以期研究在轨机动的影响、热分析和热试验时机动模式的简化模拟。通过合理地分析与简化,建立终端的轨道热分析模型,准确模拟在轨机动,根据典型机动模式、外热流和涂层退化等因素设计了计算工况,得出了终端在轨运行过程中的温度场随时间和姿态变化规律。结果表明:不同机动模式下的温度变化存在差异,最大可达23.0℃,采用固定姿态或一维转动的简化热分析或热试验不能准确模拟实际飞行温度,甚至不能部分替代二维转动热分析或热试验;光学天线和反射镜的温度控制是制约终端工作的瓶颈,为终端设计合适的避光机动策略,可大幅度提高温度稳定度和均匀度。研究结果可以为光机电设备在轨机动策略的设计和改进提供参考。 相似文献
4.
Yongjie Ding Jia Boyang Hezhi Sun Liqiu Wei Wuji Peng Peng Li Daren Yu 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2018,61(3):837-843
Discharge characteristics of a non-wall-loss Hall thruster were studied under different channel lengths using a design based on pushing a magnetic field through a double permanent magnet ring. The effect of different magnetic field intensities and channel lengths on ionization, efficiency, and plume divergence angle were studied. The experimental results show that propellant utilization is improved for optimal matching between the magnetic field and channel length. While matching the magnetic field and channel length, the ionization position of the neutral gas changes. The ion flow is effectively controlled, allowing the thrust force, specific impulse, and efficiency to be improved. Our study shows that the channel length is an important design parameter to consider for improving the performance of non-wall-loss Hall thrusters. 相似文献
5.
可控的过失速机动是先进战斗机超机动性能的重要标志,飞机飞行包线的扩大已超出传统的大气数据系统测量范围,可靠的迎角、侧滑角、总压、静压等飞行大气数据是制约先进战斗机过失速机动中飞行控制的关键因素。以中国推力矢量验证机为对象,基于过失速机动飞行试验的数据,开展大气参数估计与验证研究。结合过失速机动的时间与空间特性,研究了基于风速、地速、空速矢量和惯性姿态、导航参数的大气参数融合计算方法;针对过失速大迎角状态下飞机周围气流非定常、模型非线性导致的融合大气参数误差的复杂特性,进一步构建深度神经网络,对机动状态融合迎角、侧滑角的强非线性误差进行拟合。仿真和飞行试验表明:该方法可在大迎角飞行状态下实现主要大气参数的融合估计,过失速机动过程中融合迎角误差优于2.3°,融合得到的大气参数可为过失速大迎角机动飞行控制提供可靠的大气参数状态反馈。 相似文献
6.
The hierarchical porous N/O co-functionalized carbon(HPNOC)was scalably prepared by using the lowcost and renewable blighted grains as the raw material coupled with mild KHCO_3 activation for electrochemical capacitors(ECs).The elemental N was in situ doped in the obtained HPNOC without any N-containing additives.Remarkably,the obtained HPNOC was endowed with a large specific surface area(about 2 624m~2·g~(-1)),high pore volume(about 1.35cm~3·g~(-1)),as well as high-content N/O functionalization(about 1.9%(in atom)N and about 10.2%(in atom)O.Furthermore,the as-resulted HPNOC electrode with a high mass loading of 5mg·cm~(-2 )exhibited competitive gravimetric capacitances of about 373.6F·g~(-1 )at 0.5A·g~(-1),and even about 260.4F·g~(-1 )at a high rate of 10A·g~(-1);superior capacitance retention of about 98.8%at 1A·g~(-1 )over 10 000consecutive cycles;and high specific energy of about 9.6W·h·kg~(-1 )at a power of 500W·kg~(-1),when evaluated as a promising electrode in 6mol KOH for advanced electrochemical supercapacitors.More encouragingly,the green synthetic strategy we developed holds a huge promise in generalizing for other biomass-derived carbon materials for versatile energy-related applications. 相似文献
8.
为了研究冰冻天体表面撞击坑的形成与演化,开展了水冰的超高速撞击成坑实验。使用二级轻气炮发射1.0 mm直径的球形弹丸,以3 km/s、5 km/s和7 km/s速度对圆柱状冰块进行撞击。弹丸材料包括聚碳酸酯和不锈钢两种,冰块温度为253 K。实验观察到了不同弹丸和不同速度条件下,冰块中撞击坑的形貌特征。对撞击坑直径、深度和剖面形状进行了测量,并与文献中铝弹丸对水冰的撞击坑进行了比较分析。获得了水冰撞击坑特征随撞击参数的变化规律,结果表明:撞击坑直径和深度的主导机制不同,坑深主要由弹丸侵彻作用形成,而坑径主要由冰块的剥落所致;坑深比坑径具有更强的对于弹丸密度的依赖性,高密度弹丸撞击坑直径具有比低密度弹丸更强的对于撞击速度的依赖性;撞击坑体积与撞击能量成正比,高密度弹丸形成的撞击坑直径表现出“能量缩比”行为,而低密度弹丸形成的撞击坑直径表现出“动量缩比”行为。 相似文献
9.
Pengbin Guo Jian Sun Shuling Hu Ju Xue 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2018,61(3):787-798
Pulsar navigation is a promising navigation method for high-altitude orbit space tasks or deep space exploration. At present, an important reason for restricting the development of pulsar navigation is that navigation accuracy is not high due to the slow update of the measurements. In order to improve the accuracy of pulsar navigation, an asynchronous observation model which can improve the update rate of the measurements is proposed on the basis of satellite constellation which has a broad space for development because of its visibility and reliability. The simulation results show that the asynchronous observation model improves the positioning accuracy by 31.48% and velocity accuracy by 24.75% than that of the synchronous observation model. With the new Doppler effects compensation method in the asynchronous observation model proposed in this paper, the positioning accuracy is improved by 32.27%, and the velocity accuracy is improved by 34.07% than that of the traditional method. The simulation results show that without considering the clock error will result in a filtering divergence. 相似文献