全桥变换器中寄生参数对传导干扰的影响

以全桥变换器为例，对其主要元器件的寄生参数进行测试，运用CADENCE软件提取印刷电路板上主要印制线的寄生参数。本文分析了全桥变换器主要寄生参数对电路噪声的影响，为开关型变换器的电磁兼容性研究打下了良好的基础。在SABER仿真环境中对传导性电磁干扰的噪声进行了仿真，结果表明，寄生参数对噪声的影响明显。     

ISEE plasma observations near the subsolar magnetopause

The early ISEE orbits provided the opportunity to study the magnetopause and its environs only a few Earth radii above the subsolar point. Measurements of complete two-dimensional ion and electron distributions every 3 or 12 s, and of three-dimensional distributions every 12 or 48 s by the LASL/MPI instrumentation on both spacecraft allow a detailed study of the plasma properties with unprecedented temporal resolution. This paper presents observations obtained during four successive inbound orbits in November 1977, containing a total of 9 magnetopause crossings, which occurred under widely differing orientations of the external magnetic field. The main findings are: (1) The magnetosheath flow near the magnetopause is characterized by large fluctuations, which often appear to be temporal in nature. (2) Between 0.1 and 0.3R _E outside the magnetopause, the plasma density and pressure often start to gradually decrease as the magnetopause is approached, in conjunction with an increase in magnetic field strength. These observations are in accordance with the formation of a depletion layer due to the compression of magnetic flux tubes. (3) In cases where the magnetopause can be well resolved, it exhibits fluctuations in density, and especially pressure and bulk velocity around average magnetosheath values. The pressure fluctuations are anticorrelated with simultaneous magnetic field pressure changes. (4) In ope case the magnetopause is characterized by substantially displaced electron and proton boundaries and a proton flow direction change from upwards along the magnetopause to a direction tranverse to the geomagnetic field. These features are in agreement with a model of the magnetopause described by Parker. (5) The character of the magnetopause sometimes varies strongly between ISEE-1 and -2 crossings which occur 1 min apart. At times this is clearly the result of highly non-uniform motions. There are also cases where there is very good agreement between the structures observed by the two satellites. (6) In three of the nine crossings no boundary layer was present adjacent to the magnetopause. More remarkably, two of the three occurred while the external magnetic field had a substantial southward component, in clear contradiction to expectations from current reconnection models. (7) The only thick (low-latitude) boundary layer (LLBL) observed was characterized by sharp changes at its inner and outer edges. This profile is difficult to reconcile with local plasma entry by either direct influx or diffusion. (8) During the crossings which showed no boundary layer adjacent to the magnetopause, magnetosheath-like plasma was encountered sometime later. Possible explanations include the sudden formation of a boundary layer at this location right at the time of the encounter, and a crossing of an inclusion of magnetosheath plasma within the magnetosphere. (9) The flow in the LLBL is highly variable, observed directions include flow towards and away from the subsolar point, along the geomagnetic field and across it, tangential and normal to the magnetopause. Some of these features clearly are nonstationary. The scale size over which the flow directions change exceeds the separation distance (several hundred km) of the two spacecraft.     

交流发电机电压调节器负载电流限制电路的研究

发电机负载电流限制对保护飞机电源系统安全工作有重要意义，控制发电机励磁系统可以较灵活地实现这一功能。本文在发电机电压调节器励磁控制的基础上，提出增加一套负载电流限制电路的方案，并为某型飞机电压调节器设计出负载电流限制电路。理论分析和实验表明：该电路克服了已有电路影响调压精度的缺点，能可靠地将发电机输出短路电流限制在3倍额定值，获得理想的飞机电源系统输出外特性。     

3 kVA高频软开关航空静止变流器并联模块研究

采用公用电压外环方案，实现了三台1KVA基于频零电压开关航空静止变流器模块的并联输出，三台航空静止变流器模块均为电压，电流双环控制，通过公用电压调节器稳定并联系统的输出电在及频率，同时产生统一的模块电流给定信号，各并联模块工作电流跟踪模态，从而实现各航空静止变流器模块的均流并联，该并联方案仅有一条均流控制线连接且无须外加均流控制电路，不需要输出隔离变压器以及复杂的均流控制电路，具有简单可靠，均流精度高，体积小，重量轻和组合方便等优点，可以有效地提高航空静止变流器的可靠性，可扩展性及可维护性。     

采用重复控制器的逆变电源数字控制方案

重复控制理论是抑制谐波干扰的一种有效方法，但在逆变电源系统中，由于模型的不精确，常规方法的基于完美对消思想设计的重复控制器不适用于电源系统，针对不精确的模型，本文提出了基于部分对消思想的重复控制器设计，文中首先分析了重复控制器对谐波的抑制机理，并证明了它的稳定性和收敛性，其次给出了控制器设计的具体步骤，并给出了相应的仿真和实验验证。     

Attitude pointing enhancement for combined energy and attitude control system

This paper extends the previous works that appeared in Acta Astronautica. An approach that incorporates the Active Force Control (AFC) technique into a conventional Proportional-Derivative (PD) controller is proposed for a 50 kg small satellite. Numerical treatments are performed to validate the effectiveness of AFC. The attitude control capability of the combined energy and attitude control system (CEACS) is expected to improve. The result shows an important attitude pointing enhancement for the CEACS attitude control task.