共 45 条
- [3] Badawy A, 2006, P INT CONTR C GLASG, P1
- [5] TERMINAL GUIDANCE SYSTEM FOR SATELLITE RENDEZVOUS [J]. JOURNAL OF THE AEROSPACE SCIENCES, 1960, 27 (09): : 653 - &
- [8] Gong BC, 2018, ASTRODYNAMICS-CHINA, V2, P217, DOI 10.1007/s42064-018-0022-0
- [9] Spacecraft output feedback attitude control based on extended state observer and adaptive dynamic programming [J]. JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS, 2019, 356 (10): : 4971 - 5000