上海交大研究生院主页平台管理系统邵晓巍--中文主页-- Orbit–attitude dynamics and control of spacecraft hovering over a captured asteroid in the earth

论文成果

当前位置: 中文主页 >> 科学研究 >> 论文成果 >> Orbit–attitude d...

Orbit–attitude dynamics and control of spacecraft hovering over a captured asteroid in the earth–moon system

上一条： PRESCRIBED-TIME TIME-VARYING SLIDING MODE BASED INTEGRATED TRANSLATION AND ROTATION CONTROL FOR SPACECRAFT FORMATION FLYING

下一条： Non-singular fixed-time pose tracking control for spacecraft with dead-zone input