Developing Kepler's Law of Orbits发展开普勒轨道定律
Law of Orbits: two masses orbiting each other in bound orbits under the influence of the law of gravity will follow elliptical orbits about the center of mass of the two-body system.
轨道定律:在重力定律作用下,两个质量绕双体系统质心做有界轨道运动时,它们的轨道将遵循椭圆轨道。 The individual vector coordinates of the masses can be expressed in terms of the reduced mass: ![]() 各质量的矢量坐标可以表示为约化质量: Kepler's Laws depend upon the principle of conservation of angular momentum, and since these are inherently vector quantities, the angular momentum is expressed in terms of vector products. The angular momentum of the two body system can be expressed in terms of their relative velocity and the reduced mass of the system. Starting with the individual angular momenta, the angular momentum of the system L can be expressed as follows: ![]() 开普勒定律依赖于角动量守恒原理,由于这些量本质上是矢量,因此角动量以矢量积的形式表达。两个体系统的角动量可以表示为它们的相对速度和系统约化质量的函数。从个体的角动量开始,系统的角动量L可以表示如下: This provides the necessary framework for showing that angular momentum is conserved for an orbiting planet or a member of a binary star system. This is done by showing that the derivative of the angular momentum is zero for the case where the force of attraction acts along the line between the two bodies. This requires the expression for the derivative of a product of functions. Using the expression for angular momentum L obtained above:
这为证明角动量在行星轨道运动或双星系统成员中的守恒提供了必要的框架。这是通过展示当吸引力沿两个天体之间的连线作用时,角动量的导数为零来实现的。这需要对函数乘积的导数进行表达。利用上文得到的角动量L的表达式: The determination that the motion of both masses in a bound binary system execute elliptical orbits about a focus point at the center of mass of the system requires the analysis of the force and angular momentum of the system. The angular momentum L of the system can be expressed as ![]() 确定双星系统中两个质量的运动相对于系统质心处的焦点点执行椭圆轨道需要对系统的力和角动量进行分析。系统的角动量L可以表示为 In this expression, the unit vectors in the r direction have been introduced because both the magnitude of r and its direction can change. Note that one term drops out of the vector product expression because it contains the vector product of the unit vector and itself and is therefore zero. 在这个表达式中,引入了r方向的单位矢量,因为r的大小和方向都可以发生变化。需要注意的是,向量积表达式中有一项因包含单位矢量与自身的向量积而被消去,因此为零。 The acceleration of the reduced mass is given by ![]() 简化的质量的加速度由 where M is the total mass of the system. As a strategy for obtaining an expression for r, the following evaluation is made: ![]() 其中,M 是系统的总质量。为了获得 r 的表达式,采用以下评估方法: where the facts that the scalar product of two unit vectors is equal to 1 and the scalar product of the unit vector and its derivative is equal to 0 are used in addition to the vector identity. 其中还利用了两个事实:两个单位矢量的标量积等于1,以及单位矢量与其导数的标量积等于0的矢量恒等式。 Continuing a strategy directed toward finding an expression for radius vector r in terms of the angular momentum, the above expression is modified so that it is an equality of two derivatives. The rule for differentiation of a product is used along with the fact that dL/dt=0 (conservation of angular momentum). ![]() 继续采用寻找半径矢量r的表达式的方法,上述表达式被修改为两个导数的等式。在求导过程中使用乘积法则,并利用dL/dt=0(角动量守恒)的事实。 Now integrating the two differential quantities gives ![]() 现在将这两个微分量进行积分 where we can argue that the vector constant of integration D must be in the plane of the orbit since the other two quantities lie in that plane. To introduce the radius vector r into this expression the following procedure with a vector identity is followed. ![]() 其中我们可以论证,由于其他两个量位于该平面内,因此矢量积分常数D必须位于轨道平面内。为了将半径矢量r引入此表达式中,采用以下矢量恒等式进行处理。 Using the final expression for angular momentum L from above, this can be put in the form ![]() 利用上文中的角动量 $ L $ 的最终表达式,可以将其写成 The final step in showing that this is the expression for a conic section orbit is to define e=D/GMμ so that the radius r becomes ![]() 要证明这是圆锥曲线轨道的表达式,最后一步是定义 e = D/(GMμ),使得半径 r 变为 This form for the equation of a conic section expresses it in terms of the angular momentum L, the eccentricity e, and the angle θ measured from the perihelion. For e<1 this is the form of an ellipse and can be expressed in terms of the semimajor axis a. ![]() 这种形式的圆锥曲线方程是以角动量 L、离心率 e 和从近日点测量的角度 θ 表达的。对于 e < 1,这表示一个椭圆,可以表示为半长轴 a。 Setting these two expressions equal to each other gives an expression for the angular momentum L ![]()
将这两个表达式相等设定,得到角动量 $ L $ 的表达式 |
Index Gravity concepts Orbit concepts Carroll & Ostlie Sec 2.3 索引 重力概念 轨道概念 卡罗尔与奥斯特利埃 第2章第3节 | ||||||||
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Developing Kepler's Law of Areas发展开普勒面积定律
The velocity is in the plane of the ellipse and can be divided into radial and angular components: ![]() ![]() ![]() ![]() 速度位于椭圆平面内,可以分解为径向分量和角向分量:注意,角向分量与面积的变化率成正比,因此注意半径r和角速度相互垂直,因此它们的乘积等于它们矢量积的大小。但已在轨道定律的推导中证明,这个矢量积与角动量L成正比。也已在轨道定律的推导中证明,角动量L是一个常数,因此可以确定,对于轨道的任何一部分,面积的变化率都是常数,这就是面积定律。 |
Index Gravity concepts Orbit concepts Carroll & Ostlie Sec 2.3 索引 重力概念 轨道概念 卡罗尔与奥斯特利埃 第2章第3节 | ||
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Development of The Law of Periods轨道周期定律的发展
Law of Periods: The Law of Areas shows that the rate of change of area is proportional to the angular momentum L, and the development of the Law of Orbits showed that the angular momentum is a constant for the orbit. That rate of change of area can be integrated over time to obtain the period P. ![]() ![]() ![]() ![]() 轨道定律:面积定律表明,面积的变化率与角动量L成正比,而轨道定律的发展表明,角动量对于轨道是恒定的。该面积的变化率可以对时间积分得到周期P。由于椭圆的面积是A=πab,因此周期P遵循的关系是。现在利用轨道定律和椭圆的几何关系,其中M是总质量m1 + m2,周期表达式简化为 This establishes Kepler's Law of Periods. In this form it is useful for calculation of the orbital period of moons or other binary orbits like those of binary stars. 这种形式在计算月球或其它二体轨道(如双星系统)的轨道周期时很有用。
这确立了开普勒的周期定律。 |
Index Gravity concepts Orbit concepts Carroll & Ostlie Sec 2.3 索引 重力概念 轨道概念 卡罗尔与奥斯特利埃 第2章第3节 | ||
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