메뉴 건너뛰기




Volumn , Issue , 2000, Pages

Aeroelastic vehicle sensor placement for feedback control applications using phase stability

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTICITY; AIRCRAFT MANUFACTURE; AIRFRAMES; OPTIMIZATION; PHASE STABILITY; STABILITY CRITERIA; STEEPEST DESCENT METHOD;

EID: 85087605805     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-4148     Document Type: Conference Paper
Times cited : (13)

References (11)
  • 1
    • 0003836501 scopus 로고
    • Boeing Commercial Airplane Group, NASA-CR-4233, Langley Research Center, Hampton, Virginia, September
    • Boeing Commercial Airplane Group, "High Speed Civil Transport Study," NASA-CR-4233, Langley Research Center, Hampton, Virginia, September, 1989.
    • (1989) High Speed Civil Transport Study
  • 3
    • 1842613861 scopus 로고
    • Conventional Flight Control for an Aeroelastic Relaxed Stability High Speed Transport
    • Baltimore, Maryland, August
    • Newman, B. and Buttrill, C. "Conventional Flight Control for an Aeroelastic Relaxed Stability High Speed Transport," Proceedings of the AIAA Guidance, Navigation and Control Conference, Baltimore, Maryland, August, 1995, pp. 717-726.
    • (1995) Proceedings of the AIAA Guidance, Navigation and Control Conference , pp. 717-726
    • Newman, B.1    Buttrill, C.2
  • 6
    • 0026743764 scopus 로고
    • Method for Optimal Actuator and Sensor Placement for Large Flexible Structures
    • January-February
    • Lim, K. B., "Method for Optimal Actuator and Sensor Placement for Large Flexible Structures," Journal of Guidance, Control and Dynamics, Vol. 15, No. 1, January-February, 1992, pp. 49-57.
    • (1992) Journal of Guidance, Control and Dynamics , vol.15 , Issue.1 , pp. 49-57
    • Lim, K.B.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.