作者: Hans-Jürgen Hotop
DOI: 10.1016/S0065-2539(08)60144-4
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摘要: Publisher Summary This chapter outlines a part of different Kalman filter algorithms, with regard to their computer time usage and numerical stability. A new algorithm is presented in the advantage over conventional formulations discussed. In recent years, technique has been used for more applications, example, speech parameter estimation, image processing, traffic control, control turbines, tracking problems, etc. The basic application support inertial navigation systems. short introduction navigation, radio combination these systems shall explain problems examination development algorithm. provides comparison various by evaluation highly accurate reference path data aircraft usage. this case, simulation as well real flight radar utilized.