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	Fuel-optimal attitude maneuver using linear pseudo-spectral model predictive control method [线性伪谱模型预测能量最优姿态机动控制方法]
	Feng, Y.; Chen, W.; Yang, L.
刊名	Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
	2018
卷号	44页码:2165-2175
关键词	Attitude control Equations of motion Fuels Intelligent systems Monte Carlo methods Nonlinear equations Numerical methods Predictive control systems Real time control Trajectories Fuel optimal Gauss pseudo-spectral methods Large angle attitude maneuvers Linear quadratic regulator Numerical calculation Propagation equations Pseudo spectrum Trajectory tracking Model predictive control
ISSN号	10015965
DOI	10.13700/j.bh.1001-5965.2017.0770
URL标识	查看原文
收录类别	EI ; CSCD
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/5929899
专题	北京航空航天大学
推荐引用方式 GB/T 7714	Feng, Y.,Chen, W.,Yang, L.. Fuel-optimal attitude maneuver using linear pseudo-spectral model predictive control method [线性伪谱模型预测能量最优姿态机动控制方法][J]. Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics,2018,44:2165-2175.
APA	Feng, Y.,Chen, W.,&Yang, L..(2018).Fuel-optimal attitude maneuver using linear pseudo-spectral model predictive control method [线性伪谱模型预测能量最优姿态机动控制方法].Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics,44,2165-2175.
MLA	Feng, Y.,et al."Fuel-optimal attitude maneuver using linear pseudo-spectral model predictive control method [线性伪谱模型预测能量最优姿态机动控制方法]".Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics 44(2018):2165-2175.

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