메뉴 건너뛰기




Volumn 28, Issue 1, 2007, Pages 69-76

Entry control using sliding modes and state observer synthesis for reusable launch vehicle

Author keywords

Entry; Flight control; Multiple time scale; Robustness; Sliding mode control; State observer

Indexed keywords

AERODYNAMICS; FLIGHT CONTROL SYSTEMS; REENTRY; ROBUSTNESS (CONTROL SYSTEMS); SWITCHING;

EID: 34248336280     PISSN: 10001328     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article
Times cited : (17)

References (12)
  • 1
    • 0037265934 scopus 로고    scopus 로고
    • Onboard generation of three-dimensional constrained entry trajectories
    • Shen Z. Onboard generation of three-dimensional constrained entry trajectories[J]. Journal of Guidance, Control, and Dynamics, 2003, 26(1): 111-121
    • (2003) Journal of Guidance, Control, and Dynamics , vol.26 , Issue.1 , pp. 111-121
    • Shen, Z.1
  • 7
    • 84896693489 scopus 로고    scopus 로고
    • RLV sliding mode control system using sliding mode observers and gain adaptation
    • AIAA paper 2003-5437
    • Hall C E, Shtessel Y B. RLV sliding mode control system using sliding mode observers and gain adaptation[R]. AIAA paper 2003-5437, 2003
    • (2003)
    • Hall, C.E.1    Shtessel, Y.B.2
  • 8
    • 34248357648 scopus 로고    scopus 로고
    • Sliding mode disturbance observer-based control for a reusable launch vehicle
    • AIAA paper 2005-6145
    • Hall C E, Shtessel Y B. Sliding mode disturbance observer-based control for a reusable launch vehicle[R]. AIAA paper 2005-6145, 2005
    • (2005)
    • Hall, C.E.1    Shtessel, Y.B.2
  • 10
    • 84959178885 scopus 로고
    • Singular perturbations and time scales in guidance, navigation and control of aerospace systems: Survey
    • AIAA paper 95-3321
    • Naidu D S, Calise A J. Singular perturbations and time scales in guidance, navigation and control of aerospace systems: survey[R]. AIAA paper 95-3321, 1995
    • (1995)
    • Naidu, D.S.1    Calise, A.J.2
  • 12
    • 33750965187 scopus 로고    scopus 로고
    • Research on the reaction control system for spacecraft re-entry flight
    • Chinese source
    • NING Guo-dong, ZHANG Shu-guang, FANG Zhen-ping. Research on the reaction control system for spacecraft re-entry flight[J]. Flight Dynamics, 2005, 23(3): 16-20 (in Chinese)
    • (2005) Flight Dynamics , vol.23 , Issue.3 , pp. 16-20
    • Ning, G.-D.1    Zhang, S.-G.2    Fang, Z.-P.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.