Author:
LIU Yu,SUN Liang,HUANG Hai,CHEN Shenyan,LI Weipeng,ZHAO Xurui
Reference34 articles.
1. Finite element modeling and modal analysis of coilable mast;Wang;Appl Mech Mater,2012
2. Johnson L, Alexander L, Fabisinski L, et al. Multiple NEO rendezvous using solar sail propulsion. Proceedings, global space exploration conference 2012; 2012.
3. Validation of a scalable solar sailcraft system;Murphy;J Spacecr Rockets,2007
4. Lake M, Hazelton C, Murphey T, et al. Development of coilable longerons using elastic memory composite material. Reston: AIAA; 2002.Report No.: AIAA-2002-1453.
5. Robust fault-tolerant attitude control for satellite with multiple uncertainties and actuator faults;Fan;Chin J Aeronaut,2020