Method for correcting backup vertical gyro of aircraft, involves determining roll estimate, and taking into account features of influence of aircraft dynamics processes on accuracy, and updating orientation quaternion in accordance with roll and pitch estimates
2023-09-04
专利权人AVIONICS MOSC SCI & PRODN COMPLEX STOCK (AVIO-Non-standard)
申请日期2023-09-04
专利号RU2023122890-A
成果简介NOVELTY - The method involves using signals from the DUS and DLU. The signals are converted using quaternions into the corresponding roll and pitch angles, and the output signals of the vertical gyro, roll and pitch are jointly processed with signals corresponding to the linear accelerations obtained by conversion. The flight parameters of the aircraft are taken into account. The signals from the DLU are additionally used for an approximate estimate of the roll angles and pitch. The calculation of the quaternion q orientations for forming roll angles and pitch is performed, and the simplified estimates of the roll and pitch are taken into account. The joint processing of roll estimates and pitch is carried out. The roll estimate is determined. The features of the influence of aircraft dynamics processes on accuracy are taken into account, and the orientation quaternion is updated in accordance with the roll and pitch estimates. USE - Method for correcting backup vertical gyro of aircraft.
IPC 分类号G01C-019/02 ; G01C-021/06 ; G01C-021/18
国家俄罗斯
专业领域信息技术
语种英语
成果类型专利
文献类型科技成果
条目标识符http://119.78.100.226:8889/handle/3KE4DYBR/20534
专题中国科学院新疆生态与地理研究所
作者单位
AVIONICS MOSC SCI & PRODN COMPLEX STOCK (AVIO-Non-standard)
推荐引用方式
GB/T 7714
KACHANOV B O,KULABUKHOV V S,TUKTAREV N A,et al. Method for correcting backup vertical gyro of aircraft, involves determining roll estimate, and taking into account features of influence of aircraft dynamics processes on accuracy, and updating orientation quaternion in accordance with roll and pitch estimates. RU2023122890-A[P]. 2023.
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