大学物理里的一个方程。 比如存在一个矢量 r=xi+yi 位失r是时间t的函数,也就是r=r(t)=x(t)i+y(t)j 或 x=x(t) y=y(t) 我们从中消去时间t,则y是x的函数,也就是 y=f(x),称为质点运动的轨道方程,或轨迹方程。
轨道方程解 tracker solution
轨道参数方程 parametric orbit equation
无砟轨道工程施工方案 CRTS
轨道约束方程 Orbit Restrain Equation
轨道动力学方程 Orbital kinetic equation
在中心势场中粒子运动轨道方程的基础上,进一步讨论粒子轨道的闭合性、稳定性。
Based on the orbit equation of particle motion in central force field, the stable property and close property of orbit were discussed.
从轨道方程出发,对影响卫星光链路接收机带宽的主要因素———多普勒频移进行了研究。
The Doppler frequency shift, the main factor restricting the bandwidth of receiver in inter satellite laser link, with orbit equations is calculated.
本文通过研究地球自转时抛体运动的轨道方程和抛体的横向偏离等,揭示了地球自转对抛体运动的影响。
The paper researches into the orbit equation of the projectile motion and the projectile crosswise deviation when the earth rotates.
It's somewhat different when we're talking about the p or the d orbitals, and we won't go into the equation there, but this will give you an idea of what we're really talking about with this radial probability distribution.
当我们讨论p轨道或者,d轨道的时候会有些不同,我们那时不会给出方程,但它会给你们一个,关于径向概率,分布的概念。
So, we can do that by using this equation, which is for s orbitals is going to be equal to dr 4 pi r squared times the wave function squared, d r.
用这个方程,对于s轨道,径向概率分布,4πr的平方,乘以波函数的平方,这很容易理解。
So we know that we can relate to z effective to the actual energy level of each of those orbitals, and we can do that using this equation here where it's negative z effective squared r h over n squared, we're going to see that again and again.
我们知道我们可以将有效电荷量与,每个轨道的实际能级联系起来,我们可以使用方程去解它,乘以RH除以n的平方,它等于负的有效电荷量的平方,我们将会一次又一次的看到它。
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