@inproceedings{3281bc52358748c2b22d3bac79682673,
title = "Optimal spacecraft attitude maneuvers via adjoint method",
abstract = "This paper studies the spacecraft attitude maneuver optimization problem. The maneuver aim is to avoid fuel cost by only using CMGs in the maneuver course. The nonlinear dynamic equations of the attitude system are established, the attitude maneuver optimization is depicted into a two point boundary value problem (TPBVP). The adjoint method is used to convert the TPBVP into the initial value problem. Numerical results indicate that the adjoint method is efficiently capable for attitude maneuver optimization.",
keywords = "Adjoint method, Attitude maneuver, Optimization, Spacecraft",
author = "Jian Guo and Yu Yao and Fenghua He and Baoqing Yang and Xingdan Wang",
year = "2013",
doi = "10.4028/www.scientific.net/AMM.275-277.778",
language = "英语",
isbn = "9783037855911",
series = "Applied Mechanics and Materials",
pages = "778--781",
booktitle = "Applied Mechanics and Materials I",
note = "2012 International Conference on Applied Mechanics and Materials, ICAMM 2012 ; Conference date: 24-11-2012 Through 25-11-2012",
}