返回舱飞行试验的配平气动特性可从舱内惯性平台的加速度和姿态记录数据以及轨道数据求出。
The flight trim aerodynamic characteristics of re-entry modules were calculated from on board-recorded inertial-platform accelerations and attitudes and from reconstructed trajectory data.
根据气动力与薄膜自重和惯性力之间的动力平衡关系获得了薄膜一阶失稳时的临界风速。
The wind velocity of first order instability is obtained from the dynamic equilibrium relationship between aerodynamic force with dead weight and inertia force of membrane.
打散分级机利用离心冲击破碎原理对物料进行打散，利用惯性及空气动力学原理对散状物了实现分级。
Scatter grading device carry on using the centrifugal impact crash principle to the material scatters, to disperse the shape realization graduation using the inertia and the aerodynamics principle.
该系统的主要组件，包括一个具有表面空气动力控制的尾段，一个(身体)稳流边条套件，以及组合惯性导引系统和GPS全球定位导引控制基件。
The key components of the system consist of a tail section with aerodynamic control surfaces, a (body) strake kit, and a combined inertial guidance system and GPS guidance control unit.
BTT飞行的特点决定了控制系统存在着运动学耦合、气动耦合和惯性耦合等多种耦合因素。
The features of the BTT control method determine that its mathematical model contains many coupling elements, such as kinematical coupling, aero dynamical coupling, inertial coupling etc.
BTT飞行的特点决定了控制系统存在着运动学耦合、气动耦合和惯性耦合等多种耦合因素。
The features of the BTT control method determine that its mathematical model contains many coupling elements, such as kinematical coupling, aero dynamical coupling, inertial coupling etc.
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