TY - GEN
T1 - Optimal pose estimation with error-covariance analysis
AU - Cheng, Yang
AU - Crassidis, John L.
N1 - Publisher Copyright:
© 2021, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2021
Y1 - 2021
N2 - This paper presents a new formulation for the pose estimation problem, which involves estimating the attitude and position from vector-pair observations. It is shown that the optimal pose estimation problem is derived from a total least squares formulation. In this paper, the most general case where the covariances of the measurement errors may be fully populated matrices is considered. Then, the case where isotropic measurement errors is considered, which is related to Wahba’s problem. In both cases, it is possible to derive a loss function in terms of the unknown attitude only. The position can be determined from the estimated attitude. Error-covariances expressions for the attitude and position are derived for the isotropic-measurement case. Estimates for the vector observations, along with their respective covariances are also derived. Simulation results show that the derived covariance expressions are consistent with Monte Carlo runs.
AB - This paper presents a new formulation for the pose estimation problem, which involves estimating the attitude and position from vector-pair observations. It is shown that the optimal pose estimation problem is derived from a total least squares formulation. In this paper, the most general case where the covariances of the measurement errors may be fully populated matrices is considered. Then, the case where isotropic measurement errors is considered, which is related to Wahba’s problem. In both cases, it is possible to derive a loss function in terms of the unknown attitude only. The position can be determined from the estimated attitude. Error-covariances expressions for the attitude and position are derived for the isotropic-measurement case. Estimates for the vector observations, along with their respective covariances are also derived. Simulation results show that the derived covariance expressions are consistent with Monte Carlo runs.
UR - https://www.scopus.com/pages/publications/85100071255
M3 - Conference contribution
AN - SCOPUS:85100071255
SN - 9781624106095
T3 - AIAA Scitech 2021 Forum
SP - 1
EP - 21
BT - AIAA Scitech 2021 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2021
Y2 - 11 January 2021 through 15 January 2021
ER -