Hardware in loop simulation platform with super low disturbance torque for attitude control system of micro- and nano-satellites
LIU Yanfang1, LIU Xingfu2, QI Naiming1
1. Mechantronics Research Center for Aircraft, School of Astronautics, Harbin Institute of Technology, Harbin 150001, China; 2. Shanghai Engineering Center for Microsatellites, Shanghai 201210, China
LIU Yanfang, LIU Xingfu, QI Naiming. Hardware in loop simulation platform with super low disturbance torque for attitude control system of micro- and nano-satellites[J]. Systems Engineering and Electronics, doi: 10.3969/j.issn.1001-506X.2017.08.21.