equation-based

基本解释

For the finite propulsion reentry guidance, the conventional closed-thruster equation based on open-loop control loses its way.
摘要解决有限推力模型的再入飞行器初制导问题，利用传统开环控制的关机方程达不到要求的精度。
The results show that the VLE data can be predicted satisfactorily by theMH equation based on UNIFAC model,while the LLE data based on NRTL model.
研究结果表明：基于UNIFAC模型的MH方程能较好地预测汽液平衡，而基于NRTL模型的MH方程能满意地关联液液平衡数据。
Lyapunov Equation based algorithm for calculating state feedback gain is a comparatively normal algorithm used in pole assignment.
摘要基于李亚普诺夫方程的状态反馈增益算法是极点配置算法中比较常见的一种。
The nonlinear inversion equation based on the extended Born approximation was derived, the two-step inverse method for reconstructing the conductivity profile was presented.
基于扩展玻恩近似和电场积分方程,建立起非线性反演方程,然后应用两步线性反演方法进行迭代反演。
An equation based on thermoelasticity method with a hollow part in an uneven steady-state temperature field is derived.The equation is verified by experimental results.
用热弹性力学的方法推导了由热应力和自然膨胀所产生的孔型零件在稳态非均匀温度场中的热变形公式，实验结果也证实了公式的实用性。