This study presents a precise relative navigational method for satellites flying in formation using laser-based intermittent measurement data. The measurement data for the relative navigation between two satellites consist of a relative distance measured by a laser instrument and relative attitude angles measured by attitude determination. The relative navigation solutions are estimated by both the Extended Kalman filter (EKF) and unscented Kalman filter (UKF). The solutions estimated by the EKF may become inaccurate or even diverge as measurement outage time gets longer because the EKF utilizes a linearization approach. However, this study shows that the UKF with the appropriate scaling parameters provides a stable and accurate relative na...
The main focus of this paper is to design a more accurate optimal/suboptimal fault tolerant state e...
Navigation algorithms and the corresponding observability analysis for formation flying missions ar...
Navigation algorithms and the corresponding observability analysis for formation flying missions ar...
This paper presents relative navigation using intermittent laser-based measurement data for spacecra...
Relative navigation system is presented using GPS measurements from a single-channel global position...
This paper presents a satellite relative navigation strategy for formation flying, which chooses an ...
We made a study on real-time determination method for relative position using the laser-measured dis...
Formation flying missions involve relative navigation, or the determination of the relative kinemati...
Navigation algorithms and the corresponding observability analysis for formation flying missions are...
Navigation algorithms and the corresponding observability analysis for formation flying missions are...
Navigation algorithms and the corresponding observability analysis for formation flying missions are...
Navigation algorithms and the corresponding observability analysis for formation flying missions are...
This study developed an approach for improving Carrier-phase Differential Global Positioning System ...
Formation flying missions require autonomous relative navigation, with an accuracy depending both on...
This paper presents a robust and efficient approach for relative navigation and attitude estimation ...
The main focus of this paper is to design a more accurate optimal/suboptimal fault tolerant state e...
Navigation algorithms and the corresponding observability analysis for formation flying missions ar...
Navigation algorithms and the corresponding observability analysis for formation flying missions ar...
This paper presents relative navigation using intermittent laser-based measurement data for spacecra...
Relative navigation system is presented using GPS measurements from a single-channel global position...
This paper presents a satellite relative navigation strategy for formation flying, which chooses an ...
We made a study on real-time determination method for relative position using the laser-measured dis...
Formation flying missions involve relative navigation, or the determination of the relative kinemati...
Navigation algorithms and the corresponding observability analysis for formation flying missions are...
Navigation algorithms and the corresponding observability analysis for formation flying missions are...
Navigation algorithms and the corresponding observability analysis for formation flying missions are...
Navigation algorithms and the corresponding observability analysis for formation flying missions are...
This study developed an approach for improving Carrier-phase Differential Global Positioning System ...
Formation flying missions require autonomous relative navigation, with an accuracy depending both on...
This paper presents a robust and efficient approach for relative navigation and attitude estimation ...
The main focus of this paper is to design a more accurate optimal/suboptimal fault tolerant state e...
Navigation algorithms and the corresponding observability analysis for formation flying missions ar...
Navigation algorithms and the corresponding observability analysis for formation flying missions ar...