机载惯性导航系统仿真实验平台设计与测试

Design and Testing of Simulation Experiment Platform for Airborne Inertial Navigation System

  • 摘要: 基于FlightGear与Matlab仿真软件设计并搭建了机载惯性导航系统半实物仿真实验教学平台。该实验教学平台可通过操控飞行控制设备控制FlightGear飞行模拟软件模拟飞行,并根据生成的飞行轨迹实时生成惯性导航系统加速度计和陀螺仪传感器的仿真数据,可通过设置不同的误差参数模拟不同精度等级的惯性导航设备,基于仿真数据可开展惯性导航、惯性/卫星组合导航算法的研究。该实验教学平台可增强学生的实践动手能力以及知识应用能力,帮助学生加深对机载惯性导航系统工作原理、误差特性以及惯性/卫星组合导航的工作原理和定位性能的深入理解,还可以基于该实验平台开展惯性基导航算法的创新性实验研究,培养创新意识。

     

    Abstract: Based on FlightGear and Matlab simulation software, a half-in-the-loop simulation experiment teaching platform for airborne inertial navigation system was designed and built. The experimental teaching platform can control the flight simulation software of FlightGear flight simulation software by controlling the flight control equipment, and generate the simulation data of the accelerometer and gyroscope sensor of the inertial navigation system in real time according to the generated flight trajectory, and simulate the inertial navigation equipment of different accuracy levels by setting different error parameters, and carry out the research of inertial navigation and inertial/satellite integrated navigation algorithms based on the simulation data. The experimental teaching platform can enhance students’ practical ability and knowledge application ability, help students deepen their in-depth understanding of the working principle and error characteristics of airborne inertial navigation system, the working principle and positioning performance of inertial/satellite integrated navigation, and can also carry out innovative experimental research on inertial-based navigation algorithms based on the experimental platform to cultivate innovation consciousness.

     

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