为了减小现有小型旋翼类无飞机飞行过程中卫星/惯性组合导航系统的制导误差,提高其导航系统定位精确度,提出2维位置敏感探测器激光制导与机载卫星/惯性组合导航系统结合的新型导航系统方案。该系统利用1064nm红外脉冲激光作为引导光源,采用中间飞行段卫星/惯性导航、末端飞行段激光照射制导结合的方式,进行了理论分析和对比实验验证。结果表明,在室外飞行环境和室内强、弱、正常光照飞行环境下,该系统始终保持较高的定位精度和结果一致性；相对比其它现有制导方式,该系统的探测频率始终保持5kHz、定位精度始终保持其圆形概率误差处于0.10m数量级,取得了较好的定位实验结果。该系统具有鲁棒性强、电路简单、探测灵活、高速精确的特征,对无人机末端制导具有重要意义。

In order to reduce the guidance error of a satellite/inertial integrated navigation system and improve its navigation and positioning accuracy, a new navigation system scheme combining position sensitive detector (PSD) laser guidance with airborne satellite/inertial integrated navigation system was proposed. In this system, 1064nm infrared pulse laser was used as the guiding light source, and the combination of satellite/inertial navigation in the middle flight segment and laser guidance in the terminal flight segment was adopted. Through theoretical analysis and comparative experiments, the results show that the system always maintains high positioning accuracy and consistent results in the outdoor flight environment and the indoor strong, weak and normal lighting flight environment. Compared with the other existing guidance methods, the detection frequency of the system always remains 5kHz, and the positioning accuracy always keeps its circular error probable at the order of 0.10m. Good positioning experimental results are obtained. The system has the characteristics of strong robustness, simple circuit, flexible detection, high speed and precision. It is of great importance to the terminal guidance of unmanned aerial vehicle.