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Volumn , Issue , 2002, Pages

Design, development and flight testing of control laws for the Indian light combat aircraft

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC STABILITY; AIRCRAFT CONTROL; CONTROL THEORY; DELTA WING AIRCRAFT; FLIGHT CONTROL SYSTEMS; FLIGHT ENVELOPES; FLIGHT SIMULATORS; LIFE CYCLE; QUALITY CONTROL; SUPERSONIC AIRCRAFT; VEHICLE PERFORMANCE; WINGS;

EID: 85048706235     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-4649     Document Type: Conference Paper
Times cited : (17)

References (6)
  • 1
    • 0033097339 scopus 로고    scopus 로고
    • A Systematic Procedure to design notch filters for structural Responses with multi-axis coupling
    • March-April
    • "A Systematic Procedure to design notch filters for structural Responses with multi-axis coupling", AIAA Journal of Guidance, Control and Dynamics, Vol. 22, No.2, pp. 349-357, March-April 1999
    • (1999) AIAA Journal of Guidance, Control and Dynamics , vol.22 , Issue.2 , pp. 349-357


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.