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
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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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