运动方程

equation of time───[天]时差；时间方程

equations of state───状态方程

equation of state───[物化][自]状态方程式

equation of times───[天]时差；时间方程

equation of states───[物化][自]状态方程式

law of motion───运动定律（等于Newton'slawofmotion）

radius of action───[航]活动半径；作用半径

Many textbooks have derivations of the equations of motion. We list some below. The discussion in Reference 3 (indeed the whole book) is very clear.───很多教科书都有运动方程的推导。在下面我们列举了一些。参考文献3(实际上是整本书)中的讨论是十分清楚的。

Finally, the paper will elicit the general equations of motion about six-DOF, considering the relative motion between the two aircraft.───最后，建立的模型中是考虑两个飞行器之间的相对运动，导出通用的六自由度运动方程。

The undisturbed electron density distribution, calculated from the quantum mechanical equations of motion is shown in yellow.───根据量子力学运动学方程的计算，无扰动的电子密度分布在图中以黄色显示。

Derive and the equations of motion for a multibody dynamic system and apply the equations in a simulation of limb motion.───为多体动力学系统推出运动的公式，运用公式于肢体的运动仿真。

Choose and write down the appropriate differential equations of motion of the particle.───选择并列出适当的质点运动微分方程。

To overcome this difficulty, the momentum equations of motion are obtained from the time integration of force equations of motion.───为了克服此一困难，可以将动力平衡运动方程式对时间积分一次而转换成动量平衡运动方程式。

The equations of motion of these systems are also derived to verify their nonlinearities.───本研究也推导了这些系统运动方程式以验证其非线性。

The normal mode theory is used to provide transient dynamic responses for the equations of motion.

The following contents are studied: Ascent equations of motion are given for the orbiter with rocket engines.

Even in this case the equations of motion cannot be integrated exactly.

The nonlinear equations of motion of planing boats of arbitrary sections in regular waves are established by ordinary strip method and solved by step-by-step method at first.

We next go on to solve these equations of motion.

A new model for sea ice dynamics is developed, based on a novel mathematical approach treating the equations of motion as constraints in an optimization problem minimizing the pressure field.

In this paper, the equations of motion are derived for a single-degree-of-freedom system with a tuned mass damper (TMD).

Using a coordinate transformation matrix, which is formed by these linearly independent mode set, the component equations of motion in generalized coordinates are derived.

The nonlinear differential equations of motion for a parachutepayload system are developed, which model the parachute suspension lines and the riser as inelastic elements.