So the effect of unsteady jet should be paid attention in aerocraft design. 在飞行器设计中,必须从安全控制的角度出发,考虑这一非定常效应的影响。
High-speed reentry aerocraft is usually with terminal guidance system. 高速再入飞行器通常具有末制导系统。
By using the method,it can effectively analyse the aerocraft Simulate Training System's failure. 将此方法运用到飞行器模拟训练系统中可有效地对该系统进行故障分析。
The aerocraft attitude control is divided into two parts: attitude stabilization and attitude track. 本文将飞行器姿态控制分为：姿态稳定和姿态跟踪两种情况加以研究。
The temperature rise of aerocraft shell resulting from aero-heating and laser irradiating is given in each flight time. 并结合飞行物体的飞行状态，计算了飞行物体受连续波激光辐照时壳体温度的时间关系。
Finally, it was applied in the fault diagnosis for aerocraft and the result of experiments is satisfactory. 将其应用在飞行器故障诊断中，取得了很好的效果。
