摘要
为了解决飞行器在大航向角误差的情况下进行飞行中对准的难题,将一种线性大航向角误差模型应用于飞行器飞行中对准的过程。详细推导了线性大航向角误差模型,设计了飞行器在大航向角误差情况下进行飞行中对准的卡尔曼滤波模型,并进行了数字仿真。仿真结果表明,线性大航向角误差模型应用于飞行器飞行中对准,能够很好地解决飞行器在大航向角误差情况下进行对准的难点,并给出了适合于大航向角误差模型的机动方式。最后,提出了线性大航向角误差模型在工程应用中的几点建议。
In order to achieve aircraft in-flight alignment(IFA) with large heading error,a linear error model with large heading error is developed.The linear error model with large heading error is derived in detail,and the Kalman Filter model was designed.Digital simulation results indicate that the leaner large heading angle error model,which is applied in aircraft IFA,is effective for large heading angle error.The aircraft maneuver schemes for large heading angle error are suggested,and several engineering advices are given in the end.
出处
《航空电子技术》
2012年第1期15-19,共5页
Avionics Technology
关键词
飞行中对准
线性大航向角误差方程
捷联式惯性导航系统
卡尔曼滤波
in-flightalignment
linear large heading angle error model
strap-down inertial navigation system
Kalman filtering
