Design of entry guidance based on strong tracking filter for reentry spacecraft

Xitong Fangzhen Xuebao / Journal of System Simulation

Volumn 19, Issue 11, 2007, Pages 2535-2538

  Yang, Jun Chun ^a   Ni, Mao Lin ^a   Hu, Jun ^a  

^a BEIJING INSTITUTE OF CONTROL ENGINEERING   (China)

Author keywords

Aerodynamic coefficients; Guidance and control; Reentry spacecraft; Strong tracking filter

Indexed keywords

EID: 34447136350     PISSN: 1004731X     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (12)