| 1. | Generalized homogeneous functions and the two - body problem
广义齐次函数和二体问题 |
| 2. | Research on two - body vibrator problem
两体振子问题的研究 |
| 3. | Two - body satellite
双体卫星 |
| 4. | In the two - body case , the approximate equations of relative motion on elliptic orbits are derived
在二体假设下，推导了椭圆轨道上相对运动方程的近似形式。 |
| 5. | Based on the two - body assumption , two methods are used to investigate the mechanism of satellite formation flying on circular or near - circular orbits
首先基于二体假设，采用两种方法系统地研究了圆或近圆轨道上卫星编队飞行的构成机理。 |
| 6. | According to the process of and characteristic of rendezvous and docking , the dynamics model comprises the three following parts : two - body dynamics model , relative dynamics model and docking dynamics model
按照交会对接的过程和特点将所需的动力学模型分为三部分来研究：二体动力学模型、航天器相对动力学模型和对接动力学模型。 |
| 7. | 2 . we made a correction of the particles " velocities due to the coulomb collision among electrons and ions ( including electrons to electrons , ions to ions and electrons to ions ) with two - body collision model [ 76 , 77 ] in our code
本文运用两体碰撞模型，对电子和电子、电子和离子、离子和离子之间两体库仑碰撞对速度的改变作了相对论性修正。 |
| 8. | The shape of o constellation is an efficient way to program the missions of regional coverage of reconnaissance satellite constellation , the methods to design o con stellation are discussed in case of two - body or j2 influence
星座构型是解决侦察卫星星座区域覆盖的有效方法，本文在二体假设和考虑地球j2项影响两种情况下对星座进行了设计。 |
| 9. | Except for be and be ( two - body ) , the r . m . s distances between two clusters and the ground binding energy show that the he structure model used is reasonable to some extent . the further exploration is necessary
从集团的均方根距离和这几个超核的基态结合能计算值来看，除了a9be和岩be两体结构外，我们所采用的a ， he结构模型在某种程度上具有一定的合理性。 |
| 10. | For probing the isospin dependence of the medium correction of two - body cross sections , the results show that the behavior of the excitation function of stopping for medium size nuclear collisions can provide cleare r information than that for heavier systems
我们的结果还表明测量中等大小质量的系统在中能重离子碰撞中的核阻止本领激发函数比测量重的系统能提供更为确切的有关两体截面介质修正的信息。 |
