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Volumn 29, Issue 5, 2003, Pages 428-433

Control law reconfiguration under control surface failure for nonlinear aircraft dynamic

Author keywords

Control law reconfigure; Control surfaces; Fault tolerant technique; Flight control; Self repair flight control system

Indexed keywords

LINEAR EQUATIONS; MATHEMATICAL MODELS; PNEUMATICS;

EID: 0041926744     PISSN: 10015965     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article
Times cited : (8)

References (9)
  • 1
    • 0041653898 scopus 로고
    • Pseudo-inverse method based control reconfiguration in self-repairing flight control system
    • Chinese source, Qin H.(ed.), Beijing: China Science and Technology Press
    • Zhang Ping, Chen Zongji. Pseudo-inverse method based control reconfiguration in self-repairing flight control system [A]. In : Qin Huashu. Proceeding of the 1995 Chinese Control Conference [C]. Beijing: China Science and Technology Press, 1995. 1746-1754 (in Chinese)
    • (1995) Proceeding of the 1995 Chinese Control Conference , pp. 1746-1754
    • Zhang, P.1    Chen, Z.2
  • 2
    • 0042655802 scopus 로고    scopus 로고
    • Application of pseudoinverse method to flight control reconfiguration
    • Chinese source
    • Shao Huazhang, Yang Zhenyu, Chen Zongji. Application of pseudoinverse method to flight control reconfiguration [J]. Control and Decision, 1999. 14(3): 281-284 (in Chinese)
    • (1999) Control and Decision , vol.14 , Issue.3 , pp. 281-284
    • Shao, H.1    Yang, Z.2    Chen, Z.3
  • 4
    • 0043156773 scopus 로고    scopus 로고
    • Aircraft failures studies and its reconfigurable control
    • Chinese source
    • Zhang Ping, Chen Zongji. Aircraft failures studies and its reconfigurable control [J]. Flight Dynamics, 1997, 15(3): 67-72 (in Chinese)
    • (1997) Flight Dynamics , vol.15 , Issue.3 , pp. 67-72
    • Zhang, P.1    Chen, Z.2
  • 5
    • 0041653897 scopus 로고    scopus 로고
    • The control redundancy and reconfiguration benefit for an aircraft's roll motion
    • Chinese source
    • Zhang Ping, Chen Zongji. The control redundancy and reconfiguration benefit for an aircraft's roll motion [J]. Flight Dynamics, 1998, 16(3): 62-67 (in Chinese)
    • (1998) Flight Dynamics , vol.16 , Issue.3 , pp. 62-67
    • Zhang, P.1    Chen, Z.2
  • 7
    • 0031995290 scopus 로고    scopus 로고
    • Reconfigurable flight control of a high incidence research model using predictive control
    • Swansea, UK
    • Huzmezan M, Maciejowski J M. Reconfigurable flight control of a high incidence research model using predictive control [A]. UKACC International Conference on CONTROL' 98 [C]. Swansea, UK, 1998. 1169-1174
    • (1998) UKACC International Conference on CONTROL'98 , pp. 1169-1174
    • Huzmezan, M.1    Maciejowski, J.M.2
  • 8
    • 0037583115 scopus 로고    scopus 로고
    • Robust variable structure controller design for fault tolerant flight control
    • Kim D, Kim Y. Robust variable structure controller design for fault tolerant flight control [J]. AIAA Journal of Guidance, Control, and Dynamics, 2000, 23(3): 430-437
    • (2000) AIAA Journal of Guidance, Control, and Dynamics , vol.23 , Issue.3 , pp. 430-437
    • Kim, D.1    Kim, Y.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.