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	A high-precision attitude coordinated control method using MEMS thruster for pico- and nano-satellite [一种皮纳卫星MEMS固体微推力器阵列联合姿态控制的高精度方法]
	Yang, B.; Li, J.
刊名	Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
	2018
卷号	44页码:1378-1386
关键词	Actuators Attitude control Costs Flywheels Global optimization Nanosatellites Numerical methods Sliding mode control Solid propellants Spacecraft propulsion Wheels Allocation matrices Attitude stability Co-ordinated control High-precision Lyapunov stability Microthruster Optimal switching Terminal sliding mode Monte Carlo methods
ISSN号	10015965
DOI	10.13700/j.bh.1001-5965.2017.0481
URL标识	查看原文
收录类别	CSCD
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/5929860
专题	北京航空航天大学
推荐引用方式 GB/T 7714	Yang, B.,Li, J.. A high-precision attitude coordinated control method using MEMS thruster for pico- and nano-satellite [一种皮纳卫星MEMS固体微推力器阵列联合姿态控制的高精度方法][J]. Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics,2018,44:1378-1386.
APA	Yang, B.,&Li, J..(2018).A high-precision attitude coordinated control method using MEMS thruster for pico- and nano-satellite [一种皮纳卫星MEMS固体微推力器阵列联合姿态控制的高精度方法].Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics,44,1378-1386.
MLA	Yang, B.,et al."A high-precision attitude coordinated control method using MEMS thruster for pico- and nano-satellite [一种皮纳卫星MEMS固体微推力器阵列联合姿态控制的高精度方法]".Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics 44(2018):1378-1386.

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