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Volumn , Issue , 2000, Pages

Flight test experience of a non-linear dynamic inversion control law on the VAAC harrier

Author keywords

[No Author keywords available]

Indexed keywords


EID: 84894479872     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (34)

References (9)
  • 3
    • 0026856998 scopus 로고
    • Nonlinear Control Law with Application to High Angle-of-Attack Flight
    • May-June
    • D J Bugajski, and D F Enns, "Nonlinear Control Law with Application to High Angle-of-Attack Flight," Journal of Guidance, Control, and Dynamics, Volume 15, Number 3, May-June 1992, pp 761-767.
    • (1992) Journal of Guidance, Control, and Dynamics , vol.15 , Issue.3 , pp. 761-767
    • Bugajski, D.J.1    Enns, D.F.2
  • 5
    • 84999027758 scopus 로고
    • Robustness of Dynamic Inversion vs. mu-Synthesis: Lateral-Directional Flight Control Example
    • Navigation, and Control Conference, Portland, Oregon, August
    • D F Enns, "Robustness of Dynamic Inversion vs. mu-Synthesis: Lateral-Directional Flight Control Example," Proceedings of the 1990 AIAA Guidance, Navigation, and Control Conference, Portland, Oregon, August, 1990.
    • (1990) Proceedings of the 1990 AIAA Guidance
    • Enns, D.F.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.