메뉴 건너뛰기





Volumn 1, Issue , 1997, Pages 113-117

Longitudinal control of an advanced combat aircraft using quantitative feedback theory

Author keywords

[No Author keywords available]

Indexed keywords

CLOSED LOOP CONTROL SYSTEMS; CONTROL SYSTEM SYNTHESIS; FIGHTER AIRCRAFT; FLIGHT DYNAMICS; MOTION CONTROL; ROBUSTNESS (CONTROL SYSTEMS); TRANSFER FUNCTIONS;

EID: 0030675573     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/acc.1997.611766     Document Type: Conference Paper
Times cited : (5)

References (6)
  • Reference 정보가 존재하지 않습니다.

* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.