Research on Aircraft Landing Based on GNSS/INS/Photogrammetry Integration Using Multi-rate Extended

来源 :第九届中国卫星导航学术年会 | 被引量 : 0次 | 上传用户:ohngahng
下载到本地 , 更方便阅读
声明 : 本文档内容版权归属内容提供方 , 如果您对本文有版权争议 , 可与客服联系进行内容授权或下架
论文部分内容阅读
  The carrier-based aircraft system is the core component of modern aircraft carrier combat system,a maritime platform for carrier-borne fighters,whether carrier aircraft can demonstrate combat power depends on the ability of the carrier-based aircraft to take off and landing.In order to improve the safety and reliability of shipboard on warship,this paper aims at GNSS/INS/Photogrammetry integrated navigation theory,discussed from the basic level of integrated navigation system on implementation and the performance of the whole positioning.The mainly research is when satellite is not available,the inertial navigation error is corrected by the positioning of the Photogrammetry,to achieve high accuracy,high reliability and data refresh rate.The multi-rate kalman filter method is used to deal with the problem of the non-equal intervals between the INS and Photogrammetry.Finally,by simulating the accuracy of the integrated navigation positioning of INS/Photogrammetry by multi-rate EKF filter,to verify the feasibility of the aircraft landing/carrier landing.
其他文献
It is necessary to measure the real-time rotation speed and the roll angle of a projectile relative to the geodetic coordinate system in order to achieve accurate guidance.To obtain the rotation speed
GNSS spoofing detection method has been widely discussed recently.Most of the detection methods assume that spoofing signal is transmitted by a single source rather than distributed sources.The detect
In this paper,a novel filter based on maximum correntropy criterion(MCC)and M-estimate theory is proposed.The MCC based Kalman filter(MKF)is developed by combining the MCC and the M-estimate theories
To overcome the linearizated errors from the state equation and observation equation based on Extended Kalman Filter(EKF),a Unscented Kalman Filter(UKF)matching algorithm using geomagnetic anomaly bas
GNSS ambiguity fixed solution can greatly improve the accuracy of GNSS/INS integrated system.But it is difficult to achieve perfect real-time dynamic single frequency cycle-slip detection merely by GN
Nowadays,geomagnetic localization has become a new locating method for pedestrian.In this paper,geomagnetic matching localization method is proposed,the result of localization is based on the correlat
At present,the majority of Android phones only support satellite positioning and cellular localization.
In SATCOM On-The-Move(SOTM)systems,an accurate pointing from moving antennas towards the communication satellite is the key to a stable signal tracking.
Smartphone based pedestrian inertial navigation system usually uses the Pedestrian Dead Reckoning(PDR)algorithm to achieve navigation and positioning.The traditional PDR algorithm requires inertial de
This paper deals with the integration problem for GNSS/INS integration navigation with the aid of vision sensor.