Then general dynamic equations of the atmosphere are obtained.
从而求得普遍的大气动力学方程。
Dynamic equations in matrix form are derived for automatic weapons.
导出了矩阵形式的自动武器动力学方程。
Using gain coefficient to derive the dynamic equations of laser systems.
利用增益系数推导激光系统的动力学方程。
The dynamic equations of motion for launch vehicle with seawater inflow are derived.
建立了进水时的载体运动方程。
The dynamic equations of the circular cylindrical shell are based upon an exact moment theory.
以有矩理论导出圆柱壳体的振动微分方程。
Dynamic equations are used in which the vertical gradient and vertical diffusion are parameterized.
利用动力学方程组，并对其中垂直梯度项和垂直扩散项进行了参数化处理。
We set up robot dynamic equations using Newton Euler method on the basis of kinematics analysis of robot.
在对机器人进行运动学分析的基础上，利用牛顿欧拉法建立机器人动力学方程。
The constitutive relations of the composite and dynamic equations of the SMA transformation were predicted.
能预测复合材料的宏观本构列式和弹性基体约束下的形状记忆合金的相变特性。
And the approximate linear solutions of the reaction dynamic equations are obtained by the theory of bifurcation.
并采用分支理论得到了反应动力学方程的近似解。
The dynamic equations developed in this paper are a set of highly nonlinear STIFF ordinary differential equations.
本文导出的动力学控制方程是高度非线性的STIFF常微分方程组。
The attitude dynamic equations of a spacecraft with flexible appendages are obtained by using the momentum theorem.
利用动量矩定理推导出带挠性伸展附件航天器的动力学方程。
In this paper, an iteration method is presented for solving the dynamic equations of rigid flexible coupling system.
该文提出了一种求解刚柔耦合系统动力学方程的迭代法。
Besides, we present the procedure for obtaining dynamic equations of general robot by using kane's dynamic eqations.
本方法解算简便，经略微修改可适用于一般关节型机器人动力学模型。
Dynamic equations controlling the thermally -driven fluid convection in a single rock crack are established in the paper.
本文建立了控制垂直裂隙中热驱动对流的动力学方程。
Lagrangian dynamic equations of a robot with kinematic constraints are derived, in which generalized constraint forces are included.
推导了具有运动约束的机器人的拉格朗日动力学方程，该方程中包含了广义约束力。
A rolling base isolation system is introduced and the computing model and dynamic equations of the isolation system are established.
介绍了一种滚动基础隔震系统，并由此建立了此隔震系统的计算模型和运动微分方程。
The proposed control scheme need neither linearly parameterize the dynamic equations of system, nor know any actual inertial parameters.
该控制方案既不需要线性系统的动力学方程的参数，也不知道任何实际的惯性参数。
The dynamic equations of the spacecraft derived above are universal and programmed and is easy to realized by the computational procedure.
得到的航天器动力学方程具有通用性和程式化的特点，便于计算机编程可视化实现。
The principle, dynamic equations of variables and design concept are given. The characteristics of this circuit are presented in this paper.
给出了此电路的工作原理、动态变量方程和设计原则等理论结果，分析了该新型电路拓扑的特点。
Analytic geometry was used as an approximate method to discuss the equilibrium values of two typical dynamic equations of Life Energy System.
用解析几何作为一种近似的方法讨论了生命能量系统动力学模型中两个典型方程解函数平衡点的求解问题。
Based on clear physical concepts, complete nonlinear dynamic equations of two-phase media are derived by using classic mechanical principle directly.
本文以清楚的物理概念，依据经典力学原理建立了两相介质完整的动力学非线性方程组。
A working process simulation model was established in accordance with the dynamic process of reciprocating compressor and the valve dynamic equations.
根据活塞压缩机的工作过程和阀片的运动方程建立了其工作的模拟模型。
The coupled dynamic equations of a spacecraft with tip mass attached flexible appendage which is deployable are obtained by using the momentum theorem.
结构复杂的航天器带有几十米、上百米大型挠性附件，附件末端还带有大质量刚体。
The model of a spatial flexible rotor beam element is presented, and the dynamic equations of spatial manipulators considering joint and link flexibility is derived.
提出了空间柔性转子梁单元模型，建立了考虑关节及杆柔性的空间机器人动力学方程。
This paper introduces the features, mechanism, mathematical model, dynamic equations of the classic chemical oscillation and some applications in chemistry and biology.
本文介绍了典型振荡反应的特点、机理、数学模型、动力学方程序及在化学和生物学中的某些应用。
The dynamic equations for the coupling system of cylindrical tank partially filled with liquid are established under horizontal excitation in micro-gravity environment.
以一种新的方法建立了在微重力环境、横向激励下圆柱贮箱液固耦合系统的动力学方程。
Some important factors are considered, which include variable mass of recoiling parts and coupling between multi body dynamic equations and interior ballistic equations.
重点考虑后坐部分变质量、多体动力学方程与内弹道方程的耦合等因素。
The creation and solution of dynamic equations and problems concerning input characteristics, transient angular frequency and analysis of amplitude response are described.
文中阐述了动力学方程的建立和求解、系统输入特性和瞬态角频、振幅响应分析等问题。
Nonlinear dynamic equations of a free-floating space robot with two manipulators and a flexible end-manipulator are established based on Lagrange and assumed mode methods.
利用拉格朗日法和假设模态方法建立了末端柔性的两臂漂浮基空间机器人的非线性动力学方程。
Nonlinear dynamic equations of a free-floating space robot with two manipulators and a flexible end-manipulator are established based on Lagrange and assumed mode methods.
利用拉格朗日法和假设模态方法建立了末端柔性的两臂漂浮基空间机器人的非线性动力学方程。
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