TY - JOUR
T1 - Crater-based attitude and position estimation for planetary exploration with weighted measurement uncertainty
AU - Zhu, Shengying
AU - Xiu, Yi
AU - Zhang, Ning
AU - Xu, Rui
AU - Cui, Pingyuan
N1 - Publisher Copyright:
© 2020 IAA
PY - 2020/11
Y1 - 2020/11
N2 - A large number of crater features exist on the surface of interplanetary bodies. Autonomous navigation based on these crater features can obtain excellent navigation performance, which is one of the most important navigation methods for future planetary exploration. This paper presents a new method to estimate the attitude and position of spacecraft based on crater measurement uncertainty. Firstly, the error distribution of craters’ localization is introduced, considering the characteristics of edge detection in crater images. Then, the error uncertainty of crater localization is described by the error ellipse and the influence of related factors on the crater localization error is analyzed. Further, in consideration of the characteristics that the localization errors are anisotropic, correlated and non-identically distributed, the weighted matrix of different craters is constructed by singular value decomposition (SVD) of the error uncertainty matrix. Thereafter the weighted matrix is integrated into the attitude and position estimation algorithm. As a result, the weighted measurement uncertainty method for crater-based pose estimation is formed. Finally, the proposed algorithm is verified by Monte Carlo simulation.
AB - A large number of crater features exist on the surface of interplanetary bodies. Autonomous navigation based on these crater features can obtain excellent navigation performance, which is one of the most important navigation methods for future planetary exploration. This paper presents a new method to estimate the attitude and position of spacecraft based on crater measurement uncertainty. Firstly, the error distribution of craters’ localization is introduced, considering the characteristics of edge detection in crater images. Then, the error uncertainty of crater localization is described by the error ellipse and the influence of related factors on the crater localization error is analyzed. Further, in consideration of the characteristics that the localization errors are anisotropic, correlated and non-identically distributed, the weighted matrix of different craters is constructed by singular value decomposition (SVD) of the error uncertainty matrix. Thereafter the weighted matrix is integrated into the attitude and position estimation algorithm. As a result, the weighted measurement uncertainty method for crater-based pose estimation is formed. Finally, the proposed algorithm is verified by Monte Carlo simulation.
KW - Attitude and position estimation
KW - Crater-based optical navigation
KW - Error ellipse
KW - Measurement uncertainty
KW - Planetary exploration
UR - http://www.scopus.com/inward/record.url?scp=85086902531&partnerID=8YFLogxK
U2 - 10.1016/j.actaastro.2020.06.033
DO - 10.1016/j.actaastro.2020.06.033
M3 - Article
AN - SCOPUS:85086902531
SN - 0094-5765
VL - 176
SP - 216
EP - 232
JO - Acta Astronautica
JF - Acta Astronautica
ER -