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本文研究了弹性飞行器敏感元件位置的设置问题，分析了敏感元件位置对弹性飞行器稳定性的影响，提出了几类飞行器自动驾驶仪敏感元件可能合适位置的选择准则。从飞行器弹性振动闭环系统方程出发研究了弹性飞行器参数优化综合的某些方法。通过算例得到控制系统返馈系数，陀螺位置，舵面位置优化综合的数值模拟结果。这些结果与该飞行器实际采用的值符合较好。
In this paper, the setting of the position of the sensor is studied. The influence of the position of the sensor on the stability of the air vehicle is analyzed. The selection criterion of possible positions of the autopilot sensor is proposed. Based on the equations of the closed-loop system of the elastic vibration of the aircraft, some methods for optimizing the parameters of the elastic aircraft are studied. Through numerical examples, numerical simulation results of feedback coefficient, gyro position and rudder position optimization are obtained. These results are in good agreement with the values actually used by the aircraft.