它是地面半实物仿真系统中的一种重要专用设备，用来模拟飞行器舵机在飞行过程中所承受空气动力力矩载荷。
It is an important half hardware-in-loop simulation equipment, which is often used to simulate the aerodynamic torque load on the missile rudder or elevon actuators in the flight.
在基于建模和仿真的飞行器设计过程中，由于客观存在的不确定性，导致了模型预测结果与真实情况的不一致。
In aircraft designing process based on modeling and simulation, there exists a vast amount of uncertainty, which causes modeling predictions to differ from reality.
由于空间环境和飞行器的限制，空间晶体生长实验的成功率较低，仿真实验是解决这一问题的有效途径。
Because of the restraint of space environment and the aerocraft, the growth of crystal experiment have a low success rate, simulation is a effective way out.
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