基于DSP与单片机双机系统的电能质量监测装置

电能质量监控装置在硬件上采用TI公司的C2000系列DSP作为主运算单元,WINBOND公司的W78E58单片机作为主要外设控制单元,在软件上使用了MATLAB算法模拟功能和uC/OS-Ⅱ嵌入式操作系统,设计出一款电能质量监测装置,对提高电能供电质量提供了保障.     

纯磁控微小卫星的姿态捕获控制研究

针对纯磁控微小卫星姿态捕获问题,提出了一种基于姿态角和姿态角速度反馈的磁
矩能量控制律。利用Matrosov定理证明了该控制律具有一致渐近稳定性,能够保证星体最终
稳定到唯一的零轨道姿态角平衡位置。结合某在研低轨纳星,分析了气动力矩作用下星体大
角度姿态捕获的纯磁控性能。仿真结果表明,所设计的能量控制律具有一致渐近稳定特性,
考虑气动力矩影响时可在一个轨道周期内完成纳星姿态捕获,控制精度较高。该控制律具有
较好的工程应用前景,对于低成本微小卫星的研制是一个有益的探索。     

The energy release of substorm and magnetic storm: Its present state and future improvements by KuaFu mission

Considering the KuaFu mission, state of the energy release of substorm and storm is simply presented and it’s improvements by KuaFu mission are investigated. The KuaFu mission will provide us an opportunity to improve our understanding of the energy release during the storm and the substorms. The two KuaFu-B satellites flying in 180° phase-lagged formation in a polar orbit will allow synoptic observations of the auroral oval, central plasma sheet, ring current and other regions. It can monitor the polar region 24/7 continuously. The advantage of the KuaFu mission is to provide the data during all phases of storm and substorm time that can be used to study the global energy release during all phases continuously. The data from auroral imager and other in-situ instruments on board KuaFu-B can be used to study the auroral dynamics and Joule heating during a storm and substorm. The data from the neutral atom imager instrument can be used to study the dynamics and the energy release in the ring current region from sudden commencement to complete storm recovery. Furthermore the data from KuaFu-A, which is around L1 point, can be used to study the interplanetary conditions along with the data from the plasma sheet to study the triggering process and energy release during a substorm. So, KuaFu mission with its continuous time monitoring facilities would enable us to make much progress towards solving the underlying problems.     

椭圆轨道卫星空间任意位置悬停的方法

对任务星施加持续的控制加速度,使其在飞行过程中相对于目标卫星的空间位置保持不变,即实现任意位置悬停飞行。通过对任务星与目标星的相对运行分析和重力差异补偿分析,给出了在飞行过程中任务星相对于运行在椭圆轨道上的目标星实现任意位置悬停所需的径向、切向和法向控制加速度公式。最后对典型悬停飞行过程进行了动力学仿真,并对不同悬停飞行任务的能量消耗进行了对比分析,表明在一段时间内对任务星进行轨道悬停是可行的。     

太阳风向磁层输入电磁能量研究

利用全球磁流体力学（MHD）模拟结果,通过确立包含磁层顶的太阳风流线内边界来识别三维磁层顶位形,并以极尖区位置作为磁层顶日侧与夜侧的分界线,在此基础上定量研究了不同条件下穿过磁层顶向磁层内输入的电磁能量. 研究发现,磁层顶的能量传输与太阳风条件密切相关,磁重联是控制电磁能量传输的重要机制. 结果表明,当IMF（行星际磁场）南向时,极尖区后方的磁尾附近存在电磁能输入最大值,当IMF北向时,电磁能输入最大值发生在极尖区附近;南向IMF条件下,在IMF强度增大或太阳风密度增大时,磁层顶电磁能传输的电磁能量比北向IMF条件时增加更显著. 太阳风通过调节磁层顶面积间接影响到磁层顶能量传输大小. 研究还发现,北向IMF与南向IMF条件下穿过磁层顶的电磁能输入的比值范围约为10%～30%,此比值一定程度上反映了北、南方向IMF与地磁场磁重联效率的比值.     

Low light intensity effects on the growth,photosynthetic characteristics,antioxidant capacity,yield and quality of wheat (Triticum aestivum L.) at different growth stages in BLSS

Minimizing energy consumption and maximizing crop productivity are major challenges to growing plants in Bioregenerative Life Support System (BLSS) for future long-term space mission. As a primary source of energy, light is one of the most important environmental factors for plant growth. The purpose of this study is to investigate the effects of low light intensity at different stages on growth, pigment composition, photosynthetic efficiency, biological production and antioxidant defence systems of wheat (Triticum aestivum L.) cultivars during ontogenesis. Experiments were divided into 3 intensity-controlled stages according to growth period (a total of 65 days): seedling stage (first 20 days), heading and flowering stage (middle 30 days) and grain filling stage (last 15 days). Initial light condition of the control was 420 μmol m⁻² s⁻¹ and the light intensity increased with the growth of wheat plants. The light intensities of group I and II at the first stage and the last stage were adjusted to the half level of the control respectively. For group III, the first and the last stage were both adjusted to half level of the control. During the middle 30 days, all treatments were kept the same intensity. The results indicated that low-light treatment at seedling stage, biomass, nutritional contents, components of inedible biomass and healthy index (including peroxidase (POD) activity, malondialdehyde (MDA) and proline content) of wheat plants have no significant difference to the control. Furthermore, unit kilojoule yield of group I reached 0.591 × 10⁻³ g/kJ and induced the highest energy efficiency. However, low-light treatment at grain filling stage affected the final production significantly.     

后加载叶型叶栅的三维压力场及其对损失发展的影响

在低速环形叶栅风洞上对具有后部加载叶型的常规直叶片叶栅和弯曲叶片叶栅进行了吹风实验，得到了两种叶栅的叶片和上、下端壁表面的静压系数分布及气动性能。实验结果表明，后部加载叶型能够建立对应优良气动特性的叶栅内部三维压力场，同时采用弯叶片技术可进一步优化展向静压系数分布。     

Review of hybrid electric powered aircraft,its conceptual design and energy management methodologies

The paper overviews the state-of-art of aircraft powered by hybrid electric propulsion systems. The research status of the design and energy management of hybrid aircraft and hybrid propulsion systems are further reviewed. The first contribution of the review is to demonstrate that, in the context of relatively underdeveloped electrical storage technologies, the study of mid-scale hybrid aircraft can contribute the most to both theoretical and practical knowledge. Meanwhile, the profits and potential drawbacks of applying hybrid propulsion to mid-scale hybrid airplanes have not been thoroughly illustrated. Secondly, as summed in the overview of design methodologies, the multi-objective optimization transcends the single-objective one. The potential of the hybrid propulsion system can be thoroughly evaluated in only one optimization run, if several objectives optimized simultaneously. Yet there are few researches covering the conceptual design of hybrid aircraft using multi-objective optimization. The review of the most popular energy management strategies discloses the third research gap—current methodologies favoured in hybrid ground vehicles do not consider the aircraft safety. Additionally, both non-causal and causal energy management are needed for performing a complicated flight mission with several sub-tasks.     

几种流量测量仪表的选择与节能

对国内能源系统常用的几种工业流量测量仪表实际应用选择及节能问题,简要地进行了原理分析和实际应用分析,供使用者优选流量仪表参考。     

锥形腔高能量激光能量计后向散射问题研究

高能量激光能量的准确计量对于相关研究至关重要。量热法是测量高能量激光能量的一种有效方法,其中涉及到的入射激光在能量计吸收腔内的后向散射总能量,是一个关键参量,它的准确测定与计量,将大大提高高能量激光能量计量的准确性。依据能量计内表面与入射激光相互作用的光学定律,详细推导了锥形吸收腔内入射激光光束能量的分布函数,并结合复化辛普森数值计算方法,分析和讨论了吸收腔结构一定时,环形和矩形两种不同光斑形状的高能量激光在锥形能量计吸收腔开口处的后向散射光功率密度分布和后向散射总功率以及它们对能量测量结果的影响。