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Volumn 25, Issue 1, 1991, Pages 1-9

Variable structure slewing control and vibration damping of flexible spacecraft

Author keywords

[No Author keywords available]

Indexed keywords


EID: 0002307317     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/0094-5765(91)90002-M     Document Type: Article
Times cited : (78)

References (22)
  • 1
    • 84911657254 scopus 로고
    • A mathematical problem and a spacecraft control laboratory experiment (SCOLE) used to evaluate control laws for flexible spacecraft
    • Va, NASA/IEEE Design Challenge
    • (1984) NASA SCOLE Workshop
    • Taylor1    Balakrishnan2
  • 9
    • 0023826464 scopus 로고
    • Flexible spacecraft maneuver: inverse attitude control and modal stabilization
    • (1988) Acta Astronautica , vol.17 , pp. 1-9
    • Singh1
  • 14
    • 0024037604 scopus 로고
    • Variable structure control system (VSCS) maneuvering of flexible spacecraft
    • (1988) J. Astronaut. Sci. , vol.36 , pp. 311-344
    • Mostafa1    Öz2
  • 15
    • 0025491341 scopus 로고
    • Sliding mode control of flexible spacecraft under disturbance torque
    • (1990) Int. J. Syst. Sci. , vol.21 , pp. 1755-1771
    • Iyer1    Singh2
  • 20


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.