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Volumn , Issue , 1996, Pages 1-6

Optimal setpoint controller for a generic X-29A aircraft with forebody vortex nozzles

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT; BANG BANG CONTROL SYSTEMS; CLOSED LOOP CONTROL SYSTEMS; FEEDBACK CONTROL; FLOW CONTROL; MATHEMATICAL MODELS; NOZZLES; VELOCITY; VORTEX FLOW;

EID: 0030364991     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (8)

References (17)
  • Reference 정보가 존재하지 않습니다.

* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.