4STEVE T.Electroactive-polymer actuators for controlling space inflatable structures[J].Journal of Spacecraft and Rockets,2005,42(4):607-612.
5MARK L.Monitoring the integrity of filament wound structures using built-in sensor networks:Proceedings of SPIE-The International Society for Optical Engineering[C].5054,2003:222-229.
6MURAYAMA H.et al.Structural health monitoring of a full-scale composite structure with fiber-optic sensors[J].Advanced Composite Materials,2003,11(3):287-297.
7ARZBERGER S C.Elastic memory composites (EMC) for deployable industrial and commercial applications:Proceedings of SPIE-The International Society for Optical Engineering[C].2005,5762:35-47.
8AGRAWAL B N.Adaptive antenna shape control using piezoelectric actuators[J].Acta Astronautica,1997,40(11):821-826.
9BEAVERS F L.Design and testing of an elastic memory composite deployment hinge for spacecraft[R].AIAA,2002-1452.
10WILL F.Development and testing of a hinge/actuator incorporating elastic memory composites[R].AIAA,2003-1496.
