小展弦比飞机非线性气动特性风洞与飞行相关性研究

在较大迎角范围，如何由风洞试验数据预计全尺寸小展弦比飞机的非线性气动特性，并与飞行值相关，始终是国际航空界致力解决的重大问题，本项研究采用风洞试验与工程计算相结合的方法，对支架，洞壁、进气，喷流，雷诺数及静弹性等影响相关性的诸因素予以修正，并计及配平影响，从而比较准确地预计出全尺寸收音机的非线性气动特性，预计值与试飞值相比较结果验证了本项研究的可靠性和实用性。     

Who is who in Algol-land ? - Part II -

In part I (De Greve and Packet) we have investigated the occurrence of reversed phases of mass-transfer during Case A evolution in close binaries. If the initial period of a system is shorter than 1–2 days (Early Case A) the reversed phase starts before core hydrogen exhaustion of the gainer (part I). This type of evolution is characterized by at least two phases of slow mass-transfer.We have computed the evolution of four Early Case A systems with initial masses of the loser equal to 3 Mo and 5 Mo. These four systems start mass-exchange when Xc of the primary has decreased to 0.525 (75% of its initial value). They all experience two phases of slow mass-transfer.We find that both phases have about the same duration for all systems. The mass ratios are clearly distinct, being closer to unity during the first phase. In the Hertzsprung-Russell, mass-radius and mass-luminosity diagrams both components remain close to the main-sequence band during slow mass-transfer. Evolution as an Algol is ended when both components overflow their outer critical surface after a second reversal of the mass-transfer.Observed Algol systems evolving in Early Case A are scarce. A search thruogh the catalogue by Giuricin et al. gives us the following candidates: X Tri, SX Aur and V Pup. Based on their mass ratios, SX Aur can tentatively be assigned to the first phase of slow mass transfer and X Tri to the second phase. For V Pup (which is more massive) this choice can not be made with certainty.     

The transient highly excited solar flare plasma

Recent observations of the energetic particles produced in solar flares indicate that the production of electrons, with energies up to about 100 keV, is a fairly common feature of small flares. In those flares the acceleration of protons and other nuclei does not extend beyond about 1 MeV.The X-ray emission often exhibits two distinct components of which the first one is produced by non-thermal, the second by thermal electrons through bremsstrahlung collisions with the ambient ions. Along with these X rays, radio emission, in the microwave region, is observed. This radio emission is usually interpreted as due to gyrosynchrotron radiation from the same electrons.In this review a discussion is presented of the processes occurring in solar flares with special reference to the acceleration and radiation processes.     

The X-ray background 2–50 kev: A superposition of known sources,or evidence of a new component?

The contribution of the canonical Quasars to the XRB 2–50 keV is not likely to exceed 50%. Nay, consideration of X-ray selection effects results in a further reduction of the value of sensible estimators for the intensity ratio L_X/L_O; in addition, recent counts of radioloud and radio-quiet Quasars definitely limit the number of faint sources. A missing component with definite spectral properties should comprise a sizeable fraction of the XRB.     

四维超混沌射频隐身跳频通信设计方法

为提高飞行器通信系统的抗截获性能，提出了一种基于四维超混沌系统的射频隐身跳频通信设计方法。该方法构建了四维超混沌系统，扩展了系统解空间，有效增加了系统复杂度，并通过引入周期性扰动措施，解决了有限精度带来的短周期现象。在四维超混沌系统的基础上，利用超混沌系统生成的双通道超混沌序列，实现了跳频通信系统的频率序列和周期序列联合不确定设计方法。仿真结果表明：四维超混沌系统与传统混沌系统相比，其复杂度最优，在相同有限精度条件下，超混沌系统的周期性明显减弱。另外，基于四维超混沌设计的跳频系统，其截获概率优于常规跳频系统，具有较好的射频隐身性能。     

深空测控通信中GMSK体制非相干解调算法研究

针对深空测控通信中GMSK体制非相干解调损失较大的难点,提出了一种改进的GMSK信号非相干维特比解调算法。通过分析相位状态网格图中相位转移规律,建立理论仿真模型。通过原理样机的研制和测试,实测数据表明：该算法具有解调损失低、实现复杂度适中的优点;相比于理论的最佳相干解调算法,在误码率1×10 -4 量级下,实测仅损失0.6 dB。目前该算法已应用于国内某深空测控通信系统GMSK体制基带设备中,并成功解调出欧空局Herschel–Planck卫星数据。     

Effects of uncertainties and flexible dynamic contributions on the control of a spacecraft full-coupled model

One of the most important problems for performing a good design of the spacecraft attitude control law is connected to its robustness when some uncertainty parameters are present on the inertial and/or on the elastic characteristics of a satellite. These uncertainties are generally intrinsic on the modeling of complex structures and in the case of large flexible structures they can be also attributed to secondary effects associated to the elasticity. One of the most interesting issues in modeling large flexible space structures is associated to the evaluation of the inertia tensor which in general depends not only on the geometric ‘fixed’ characteristic of the satellite but also on its elastic displacements which of course in turn modify the ‘shape’ of the satellite. Usually these terms can be considered of a second order of magnitude if compared with the ones associated to the rigid part of a structure. However the increasing demand on the dimension of satellites due to the presence for instance of very large solar arrays (necessary to generate power) and/or large antennas has the necessity to investigate their effects on their global dynamic behavior in more details as a consequence. In the present paper a methodology based on classical Lagrangian approach coupled with a standard Finite Element tool has been used to derive the full dynamic equations of an orbiting flexible satellite under the actions of gravity, gravity gradient forces and attitude control. A particular attention has been paid to the study of the effects of flexibility on the inertial terms of the spacecraft which, as well known, influence its attitude dynamic behavior. Furthermore the effects of the attitude control authority and its robustness to the uncertainties on inertial and elastic parameters has been investigated and discussed.     

对解线频调ISAR的间歇采样转发干扰

针对间歇采样转发应用于宽带ISAR干扰问题,研究了间歇采样转发信号经解线频调ISAR二维成像处理后信号特性,通过推导干扰信号对应的二维输出形式,讨论了干扰图像变化情况并由此分析了间歇采样周期和占空比对干扰效果的影响。利用数字仿真验证了干扰输出形式及图像特征理论分析的正确性;将实测数据与间歇采样转发处理相结合,初步验证了间歇采样转发干扰能够形成二维ISAR假目标。     

空间机器人在轨更换ORU的力/位混合控制方法

针对ORU在轨更换任务,首先推导了空间机械臂末端自由、末端与环境接触等情况下的动力学方程,并提出了相应的接触力计算方法;其次,改进了传统的R\|C控制方法,采用加权选择矩阵代替原有的选择矩阵,实现了力控制与位置控制之间的平滑切换;最后,开发了基于Matlab/Simulink的闭环控制仿真系统,该系统由多体动力学、接触动力学、轨迹规划、力/位混合控制、3D显示等模块组成。利用该系统开展了ORU转移与安装过程的闭环控制仿真,仿真结果校验了所提方法的有效性。