@inproceedings{677fbe1b43624e4a95b2296b01a69ccd,
title = "Mass property estimation for mated flight control",
abstract = "Mass property of space vehicle changes apparently during and after mating and cannot be predicted or measured at times, yet it needs to be accurately known for mated flight control or attitude control and momentum management. A discrete Kalman Filter (KF) based estimation method is developed, measurements of single point acceleration, angular velocity and angular acceleration are employed to extract the inertia matrix and mass center. Simulation results show that the method can be used for continues online estimation without propellant consumption.",
keywords = "Estimation, KF, Mass property, Mated flight control",
author = "Zhao Yang and Zhang Dawei and Tian Hao and Li Na",
year = "2009",
doi = "10.1109/ICCMS.2009.55",
language = "英语",
isbn = "9780769535623",
series = "Proceedings - 2009 International Conference on Computer Modeling and Simulation, ICCMS 2009",
pages = "84--87",
booktitle = "Proceedings - 2009 International Conference on Computer Modeling and Simulation, ICCMS 2009",
note = "2009 International Conference on Computer Modeling and Simulation, ICCMS 2009 ; Conference date: 20-02-2009 Through 22-02-2009",
}