2014
DOI: 10.1109/tcst.2013.2255288
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Stereovision-Based Estimation of Relative Dynamics Between Noncooperative Satellites: Theory and Experiments

Abstract: Estimating the relative pose and motion of cooperative satellites using on-board sensors is a challenging problem. When the satellites are noncooperative, the problem becomes even more complicated, as there might be poor a priori information about the motion and structure of the target satellite. In this paper, the mentioned problem is solved by using only visual sensors, which measurements are processed through robust filtering algorithms. Using two cameras mounted on a chaser satellite, the relative state wi… Show more

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Cited by 149 publications
(70 citation statements)
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“…The accuracy of the proposed algorithm is significantly higher than that in Segal et al 5 Especially in the distance, there are more obvious advantages in the proposed algorithm. The attitude accuracy comparison in the same distance is shown in Table 1.…”
Section: Comparison With Existing Methodsmentioning
confidence: 71%
See 1 more Smart Citation
“…The accuracy of the proposed algorithm is significantly higher than that in Segal et al 5 Especially in the distance, there are more obvious advantages in the proposed algorithm. The attitude accuracy comparison in the same distance is shown in Table 1.…”
Section: Comparison With Existing Methodsmentioning
confidence: 71%
“…4 A number of pose estimation methods have been reported. Segal et al 5,6 developed a stereovision-based filtering algorithm for estimating the state between two non-cooperative spacecrafts. Using two cameras mounted on a chaser satellite, the relative state with respect to a target satellite, including the position, attitude, and rotational and translational velocities, is estimated.…”
Section: Introductionmentioning
confidence: 99%
“…Assumption 2: The chaser can directly measure its motion variables {r, v, σ, ω} and relative motion variables {r e , v e , σ e , ω e } with the measurement devices mounted on the chaser body [40] [41]. However, the tumbling target's motion variables {r t , v t , σ t , ω t } are assumed to be unavailable directly for the chaser.…”
Section: B Relative Motion Dynamicsmentioning
confidence: 99%
“…11). Этот стол состоит из 9 пластин размером 1х1 м 2 с отверстиями, скре-пленных друг с другом [11].…”
Section: аэродинамический стол с воздушной подушкойunclassified