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Volumn , Issue , 2003, Pages

X-45 program overview and flight test status

Author keywords

[No Author keywords available]

Indexed keywords

FLIGHT ENVELOPES; MILITARY AVIATION; SOFTWARE TESTING;

EID: 85085403528     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-6645     Document Type: Conference Paper
Times cited : (14)

References (4)
  • 3
    • 84896693766 scopus 로고    scopus 로고
    • Aeroservoelastic Design and Test of the X-45A Unmanned Combat Air Vehicle
    • Proceedings of the 44th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference, Paper AIAA 2003-1883, Norfolk
    • Reichenbach, E. Y., and Davidson, R. W., Aeroservoelastic Design and Test of the X-45A Unmanned Combat Air Vehicle", Proceedings of the 44th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference, Paper AIAA 2003-1883, Norfolk, Virginia, 7-10 April 2003.
    • (2003) Virginia , pp. 7-10
    • Reichenbach, E.Y.1    Davidson, R.W.2
  • 4
    • 84959128537 scopus 로고
    • Application of Real Structure Singular Values to Flight Control Law Validation Issues
    • AIAA-95-3190-CP
    • Miotto, P. and J. D. Paduano, "Application of Real Structure Singular Values to Flight Control Law Validation Issues", Proc. of AIAA GNC Conf., Baltimore, MD, Aug. 1995, AIAA-95-3190-CP.
    • (1995) Proc. of AIAA GNC Conf., Baltimore, MD
    • Miotto, P.1    Paduano, J.D.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.