文件名称:88276272
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系统阐述了小天体运动对应的圆型限制性三体问题共线平动点的强不稳定性特征,以及其附
近的条件周期轨道一晕轨道(HaloOrbit)的存在、相应解的构造.这种特殊的轨道形式和共线
平动点附近的弱稳定走廊,可分别用于在深空特殊位置附近定点有各种科学探测目标的探测器和向
节能轨道过渡的通道.
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Systematically expounded the small celestial motion corresponding circular restricted three-body problem collinear libration point of strong instability characteristics, and its subsidiary
Conditions of periodic orbits near a halo orbit (HaloOrbit) the existence of appropriate structural solution. This particular track forms and collinear
Libration point near weakly stable corridor can be used in deep space, respectively, near the spot a variety of special scientific exploration target detector and to
Energy orbital transition channel.
近的条件周期轨道一晕轨道(HaloOrbit)的存在、相应解的构造.这种特殊的轨道形式和共线
平动点附近的弱稳定走廊,可分别用于在深空特殊位置附近定点有各种科学探测目标的探测器和向
节能轨道过渡的通道.
-
Systematically expounded the small celestial motion corresponding circular restricted three-body problem collinear libration point of strong instability characteristics, and its subsidiary
Conditions of periodic orbits near a halo orbit (HaloOrbit) the existence of appropriate structural solution. This particular track forms and collinear
Libration point near weakly stable corridor can be used in deep space, respectively, near the spot a variety of special scientific exploration target detector and to
Energy orbital transition channel.
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关于共线平动点的特征及其在深空探测中的应用.caj