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Strategies for plane change of Earth orbits using lunar gravity and derived trajectories of family G
C. F. de Melo E. E. N. Macau O. C. Winter 《Celestial Mechanics and Dynamical Astronomy》2009,103(4):281-299
The dynamics of the circular restricted three-body Earth-Moon-particle problem predicts the existence of the retrograde periodic
orbits around the Lagrangian equilibrium point L1. Such orbits belong to the so-called family G (Broucke, Periodic orbits
in the restricted three-body problem with Earth-Moon masses, JPL Technical Report 32–1168, 1968) and starting from them it
is possible to define a set of trajectories that form round trip links between the Earth and the Moon. These links occur even
with more complex dynamical systems as the complete Sun-Earth-Moon-particle problem. One of the most remarkable properties
of these trajectories, observed for the four-body problem, is a meaningful inclination gain when they penetrate into the lunar
sphere of influence and accomplish a swing-by with the Moon. This way, when one of these trajectories returns to the proximities
of the Earth, it will be in a different orbital plane from its initial Earth orbit. In this work, we present studies that
show the possibility of using this property mainly to accomplish transfer maneuvers between two Earth orbits with different
altitudes and inclinations, with low cost, taking into account the dynamics of the four-body problem and of the swing-by as
well. The results show that it is possible to design a set of nominal transfer trajectories that require ΔV
Total less than conventional methods like Hohmann, bi-elliptic and bi-parabolic transfer with plane change. 相似文献
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在各种摄动因素的作用下,导航卫星将逐渐偏离其预定轨道,因而需要通过轨道机动的方法来予以纠正。但轨道机动后,由预报轨道所提供的轨道先验信息将失去作用,这是用星间距离观测值和先验轨道信息进行导航卫星自主定轨时必须要解决的问题。提出机动后,机动卫星采用几何法来确定自己的位置,然后用动力学法来进行轨道拟合和轨道预报,在机动后第二天就能恢复正常的自主定轨。即使有多个卫星在同一天发生机动,个别卫星因可观测卫星不足4个而无法定轨,在第二天就能实现几何法定位,不会影响整个系统的导航定位功能。 相似文献
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针对一类低轨道磁控立方星,提出一种在线加权式多模型自适应跟踪控制方法,使得卫星姿态能够根据指令实现较大角度的机动,并将误差保持在容许的范围内,达到满意的动态性能.首先,在卫星的几个姿态平衡点处建立控制系统模型,通过模型匹配度指标值,在线调整加权式多模型控制算法;其次,在多模型控制回路中引入动态自适应神经网络,充分利用其结构和参数均可以在线自适应调节的特点,以消除卫星在轨运行时受到的地球磁场变化的影响,并抑制不确定的外部干扰,提高系统鲁棒性能;最后,以某立方星为对象,进行仿真验证,结果表明所提方法是有效的. 相似文献
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This paper is the continuation of the work described in [14], dedicated to the presentation of the results of propeller performance in behind-hull during straight ahead motion obtained by a novel experimental set-up for the measurements of single blade loads. In the present case, the study shows and discusses the single blade and propeller loads developed during steady turning conditions, that were simulated by means of free running, self propelled maneuvering tests for a twin screw configuration. Maneuvering conditions are critical for the ship propulsion system, because the performance of the propeller and the side effects related to its functioning (propeller–hull induced pressure and vibrations, noise) are completely different with respect to the design condition in straight ahead motion. Thrust and torque and generation of in-plane loads (force and moments), developed by the blade during the period, evolve differently for the two propellers, due to different propeller–wake interactions. The understanding and the accurate quantification of propeller loads, in these realistic operative scenarios, are pivotal to design low emission and comfortable ships, fulfilling the requirements of safety and continuity of operations at sea. The analysis is carried out revisiting the investigation in [14] for three different speeds (FN = 0.26, 0.34 and 0.40) and a large set of rudder angles that span moderate and tight maneuvers. 相似文献
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针对水下机器人操纵性优化设计中水动力系数预报问题,在水下机器人水动力预报中引入艇体肥瘦指数概念,确定了水下机器人艇体几何描述的五参数模型。提出采用小波神经网络方法预报水下机器人水动力,确定了神经网络的结构,利用均匀试验设计方法,设计了神经网络的学习样本。研究结果表明,只要确定适当的输入参数,选择适当的学习样本和网络结构,利用小波神经网络方法对水下机器人水动力进行预报可以达到较好的精度。 相似文献
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针对北斗卫星姿轨控后的轨道快速确定难题,系统地研究了基于多项式拟合和基于星历拟合两种运动学定轨方法,推导建立了相应的运动学定轨模型。同时针对接收机系统差和顽固多径问题,利用基于并置比对的接收机系统差解算方法和CNMC的多径削弱方法,实现了超短弧跟踪条件下接收机数据质量的有效控制。利用北斗GEO/IGSO/MEO卫星的实测伪距数据进行了试验验证,结果表明在10min超短弧跟踪条件下,GEO、IGSO和MEO卫星的运动学定轨位置精度分别为3.27m、8.19m和5.90m,实现了超短弧跟踪条件下的北斗卫星快速定轨,满足了卫星机动期间的北斗RDSS服务对轨道精度的需求,为北斗RDSS服务走向全球提供了技术支撑。 相似文献
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高分辨率光学遥感卫星宽幅成像技术发展浅析 总被引：1，自引：0，他引：1
幅宽是影响高分辨率光学遥感卫星应用的重要指标。本文分析了国际上高分辨率光学遥感卫星宽幅成像的主要途径,介绍了多CCD内视场拼接、多相机外视场拼接、敏捷成像、多星组网等主流宽幅成像方式及其数据处理的技术特点,同时分析了相机垂轨摆扫成像、大面阵相机敏捷拼幅成像等新型星载宽幅影像获取方式,有助于系统地了解高分辨率光学遥感卫星宽幅成像技术进展,对于展望其发展趋势具有一定的参考作用。 相似文献
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