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61.
质子耀斑活动区的再现规律 总被引:3,自引:2,他引:1
质子耀斑活动区再现规律的研究结果表明,日面上存在着经度方向漂移式的“活火山”,即质子活动复活体,“活火山”定期地复活,并爆发质子耀斑。其复活长周期为8-11.6年,与活动周11年周期基本一致;短周期为1.26年,与活动周峰年时间宽度一致。在22周峰年中,日面南北半球上各有一个强质子活动复活体,它们爆发值流量≥100pfu和≥1000pfu的质子耀斑各占周期同类耀斑总数的70.7%和83.3%。 相似文献
62.
采用碳氢燃料冷却壁面是超燃冲压发动机常用主动冷却方式。为减轻主动冷却通道结构重量、提高冷却效率,本文探讨了以网格结构为填充的新型通道,从结构轻质化、流动特性及综合传热能力等方面与常规矩形主动冷却通道进行了比较。结果表明,在相同工况下,由错排网格填充的冷却通道结构综合性能最佳,其减重效果达39.93%,壁面温度显著下降,且努塞尔数最高达到光通道的2.156倍。从流动传热机理分析可看出,网格前缘冲击效应形成的马蹄涡和后缘附近发卡涡结构对强化传热贡献最大,扰动边界层和激发湍动能也是强化传热的重要因素。 相似文献
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针对控制力矩陀螺——主动磁轴承飞轮转子系统的强非线性和由陀螺效应产生的进动和章动导致系统的失稳问题,提出了神经网络的控制方案,设计了RBF神经网络控制器,并给出了李亚普诺夫函数的稳定性证明。研究表明,该控制器解决了陀螺效应导致的主动磁轴承-飞轮转子的不稳定性问题,且抑制了噪声对磁轴承稳定性所造成的破坏。最后,数值算例证明了该方法消除噪声的可行性和有效性。 相似文献
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67.
天线罩外形形线对天线罩性能的影响 总被引:1,自引:0,他引:1
比较和分析了不同天线平外形形线在不同长细比情况下对天线罩的电气性能和气动特性的影响。分析认为,在设计天线罩时,应根据导弹和天线罩的综合性能要求进行综合处理。 相似文献
68.
The angular motion of an axisymmetrical satellite equipped with an active magnetic attitude control system is considered. The dynamics of the satellite are analytically studied on the whole control loop. The control loop is as follows: preliminary reorientation along with nutation damping, spinning about the axis of symmetry, then precise reorientation of the axis of symmetry in inertial space. Reorientation starts right after separation from the launch vehicle. Active magnetic attitude control system time-response with respect to its parameters is analyzed. It is proven that low-inclined orbit forces low control system time-response. Comparison with the common control scheme shows the time-response gain. Numerical analysis of the disturbances effect is carried out and good pointing accuracy is proved. 相似文献
69.
M.V. Alania A. Gil R. Modzelewska 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008,41(2):280-286
We demonstrate that the general features of the radial and azimuthal components of the anisotropy of galactic cosmic rays can be studied by the harmonic analysis method using data from an individual neutron monitor with cut off rigidity <5 GV. In particular, we study the characteristics of the 27-day (solar rotation period) variations of the galactic cosmic ray intensity and anisotropy, solar wind velocity, interplanetary magnetic field strength and sunspot number. The amplitudes of the 27-day variations of the galactic cosmic ray anisotropy are greater, and the phases more clearly established, in A > 0 polarity periods than in A < 0 polarity periods at times of minimum solar activity. The phases of the 27-day variations of the galactic cosmic rays intensity and anisotropy are opposite with respect to the similar changes of the solar wind velocity in A > 0 polarity periods. No significant dependence of the amplitude of the 27-day variation of the galactic cosmic ray anisotropy on the tilt angle of the heliospheric neutral sheet is found. Daily epicyclegrams obtained by Chree’s method show that the 27-day variations of the galactic cosmic ray anisotropy during A > 0 polarity periods follow elliptical paths with the major axes oriented approximately along the interplanetary magnetic field. The paths are more irregular during A < 0 polarity periods. 相似文献
70.
《Acta Astronautica》2014,93(1):373-384
Asteroid retrieval, satellite servicing, and debris removal concepts often rely on a thrusting vehicle to redirect and steer a passive object. One effective way to tow the object is through a tether. This study employs a discretized tether model attached to six degree-of-freedom end bodies. To reduce the risk of a post-burn collision between the end bodies, discrete thrust input shaping profiles are considered including a Posicast input and a bang-off-bang thrust profile. These input shaping techniques attain desirable collision avoidance performance by inducing a tumbling or gravity gradient motion of the tethered formation. Their performance is compared to an earlier frequency notched thruster profile. 相似文献