@inproceedings{ee63ddfbf32948359db94cd86a693179,
title = "Generalized attitude determination with one dominant vector observation",
abstract = "This paper derives an algorithm to determine the approximate attitude of a vehicle from both vector and arc-length observations, which are the most general types of attitude observa-tions. It is assumed that one of the vector observations is more accurate than the other vector and arc-length observations. The solution is found by solving a quartic polynomial equation. Then the quaternion can be determined from the polynomial solution. The attitude error-covariance is also derived using both an attitude perturbation approach and a constrained least squares approach. Both are shown to yield identical results. An optimality condition is also derived that compares the derived suboptimal error-covariance with the optimal one. Several special cases, such as a set of one direction observation and an arc-length observation, are shown. Simulation results using a Monte Carlo analysis are shown to verify the derived algorithm.",
author = "Crassidis, \{John L.\} and Yang Cheng",
note = "Publisher Copyright: {\textcopyright} 2019, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; AIAA Scitech Forum, 2019 ; Conference date: 07-01-2019 Through 11-01-2019",
year = "2019",
doi = "10.2514/6.2019-1174",
language = "English",
isbn = "9781624105784",
series = "AIAA Scitech 2019 Forum",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "AIAA Scitech 2019 Forum",
}