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Applied Quaternion Optimization Method in Transfer Alignment for Airborne AHRS Under Large Misalignment Angle

机译:四元数优化方法在大偏角下机载AHRS传递对准中的应用

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摘要

The airborne attitude and heading reference system (AHRS) is an inertial system that provides the aircraft with navigation parameters in real time. A new coarse transfer alignment method is proposed for low-accuracy AHRS with a large misalignment angle between AHRS and master inertial navigation system (MINS). The new coarse alignment method is derived from the quaternion-optimization-based in-flight alignment (IFA) method. By resolving the alignment problem in body frame, the proposed method makes full use of the navigation information of MINS and transforms the alignment problem into a quaternion optimization problem. Its accuracy is improved by presenting a two-step iterative algorithm. Compared with the quaternion-optimization-based IFA method, the proposed method is more robust and accurate by introducing the attitude information of MINS. The simulation and experiment results show that the proposed method is applicable to both large and small misalignment angles, and it serves as a nice coarse alignment that permits the implementation of linear error model in fine alignment process.
机译:机载姿态和航向参考系统(AHRS)是一种惯性系统,可为飞机提供实时导航参数。针对AHRS与主惯性导航系统(MINS)之间的未对准角较大的低精度AHRS,提出了一种新的粗调对准方法。新的粗对准方法是基于基于四元数优化的飞行中对准(IFA)方法得出的。通过解决车身框架中的对准问题,该方法充分利用了MINS的导航信息,并将对准问题转化为四元数优化问题。通过提出两步迭代算法可以提高其准确性。与基于四元数优化的IFA方法相比,该方法通过引入MINS的姿态信息更加鲁棒和准确。仿真和实验结果表明,该方法适用于大偏角和小偏角,并且具有良好的粗对准效果,可以在精细对准过程中实现线性误差模型。

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