attitude determination algorithm

基本解釋

A filtering algorithm for high precision attitude determination of a specific satellite is presented based on star-sensors and fiber optic gyroscopes (FOG).
為了滿足衛(wèi)星三軸姿態(tài)確定的精度要求，提出了基于狀態(tài)估計(jì)法的星敏感器和光纖陀螺組合的方案，并設(shè)計(jì)了相應(yīng)姿態(tài)確定算法。
An adaptive extended Kalman filtering algorithm is presented in this paper for attitude determination consisting of a pseudo gyro, a magnetometer and an earth sensor.
以偽陀螺、磁強(qiáng)計(jì)與地球敏感器構(gòu)成的姿態(tài)測(cè)量系統(tǒng)為基礎(chǔ)，設(shè)計(jì)了自適應(yīng)擴(kuò)展卡爾曼濾波算法。
A novel optimal attitude and attitude-rate estimation algorithm is proposed to address the problem of autonomous attitude determination using gravitational filed and geomagnetic field observation.
針對(duì)利用地球重力場(chǎng)和磁場(chǎng)矢量觀測(cè)進(jìn)行自主姿態(tài)測(cè)量的應(yīng)用問(wèn)題，提出了一種新的最優(yōu)遞推估計(jì)算法。
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