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Volumn , Issue , 2002, Pages

Control allocation for the next generation of entry vehicles

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AERODYNAMICS; CONTROL THEORY; LINEAR PROGRAMMING;

EID: 85085776977     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-4849     Document Type: Conference Paper
Times cited : (33)

References (8)
  • 1
    • 0003771178 scopus 로고    scopus 로고
    • Flight Dynamics Directorate, Wright Laboratory, WL-TR-96-3099, Wright-Patterson Air Force Base, OH, May
    • Application of Multivariable Control theory to Aircraft Control Laws. Flight Dynamics Directorate, Wright Laboratory, WL-TR-96-3099, Wright-Patterson Air Force Base, OH, May 1996.
    • (1996) Application of Multivariable Control Theory to Aircraft Control Laws
  • 2
    • 0028388432 scopus 로고
    • Constrained Control Allocation: Three-Moment Problem
    • Durham, W.C., "Constrained Control Allocation: Three-Moment Problem," Journal of Guidance, Control, and Dynamics, Vol. 17, No. 2, 1994, pp. 330-336.
    • (1994) Journal of Guidance, Control, and Dynamics , vol.17 , Issue.2 , pp. 330-336
    • Durham, W.C.1
  • 8
    • 84896051819 scopus 로고    scopus 로고
    • NASA Flight Training Branch, TD357A, October
    • Deger, D., Entry Guidance Workbook. NASA Flight Training Branch, TD357A, October 1996.
    • (1996) Entry Guidance Workbook
    • Deger, D.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.