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Volumn 48, Issue 1, 2001, Pages 45-67

Globally asymptotically stable reorientation controller with control constraint and slew rate limit

Author keywords

[No Author keywords available]

Indexed keywords

ASYMPTOTIC STABILITY; CONSTRAINT THEORY; EQUATIONS OF MOTION; NONLINEAR CONTROL SYSTEMS; NUMERICAL METHODS; SPACE FLIGHT; TORQUE; VECTORS; ATTITUDE CONTROL;

EID: 0035067794     PISSN: 00219142     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article
Times cited : (3)

References (20)
  • 2
    • 85003405823 scopus 로고
    • Optimal continuous torque attitude maneuvers
    • May-June
    • JUNKINS, J. L. and TURNER, J. P. "Optimal Continuous Torque Attitude Maneuvers," Journal of Guidance and Control, Vol. 3, No. 3, pp. 210-217, May-June 1980.
    • (1980) Journal of Guidance and Control , vol.3 , Issue.3 , pp. 210-217
    • Junkins, J.L.1    Turner, J.P.2
  • 3
    • 0018544626 scopus 로고    scopus 로고
    • Optimal open loop maneuver profiles for flexible spacecraft
    • FARRENKOPF, R. L. "Optimal Open Loop Maneuver Profiles for Flexible Spacecraft," Journal of Guidance, Control, and Dynamics, Vol. 2, No. 6, pp. 491-498.
    • Journal of Guidance, Control, and Dynamics , vol.2 , Issue.6 , pp. 491-498
    • Farrenkopf, R.L.1
  • 4
    • 85003340103 scopus 로고    scopus 로고
    • Optimal large angle single axis maneuvers of flexible spacecraft
    • TURNER, J. D. and JUNKINS, J. L. "Optimal Large Angle Single Axis Maneuvers of Flexible Spacecraft," Journal of Guidance, Control, and Dynamics, Vol. 3, No. 5, pp. 578-585.
    • Journal of Guidance, Control, and Dynamics , vol.3 , Issue.5 , pp. 578-585
    • Turner, J.D.1    Junkins, J.L.2
  • 6
    • 0021413434 scopus 로고    scopus 로고
    • Optimal open loop and stable feedback control of rigid spacecraft attitude maneuvers
    • VADALI, S. R. and JUNKINS, J. L. "Optimal Open Loop and Stable Feedback Control of Rigid Spacecraft Attitude Maneuvers," Journal of the Astronomical Sciences, Vol. 32, No. 2, pp. 105-122.
    • Journal of the Astronomical Sciences , vol.32 , Issue.2 , pp. 105-122
    • Vadali, S.R.1    Junkins, J.L.2
  • 7
    • 85003316222 scopus 로고
    • Minimum-time large-angle reorientation of a rigid spacecraft
    • Portland, Oregon, Paper No. 90-3486, August
    • BILIMORIA, K. D. and WIE, B. "Minimum-Time Large-Angle Reorientation of a Rigid Spacecraft," AIAA Guidance, Navigation and Control Conference, Portland, Oregon, Paper No. 90-3486, August 1990.
    • (1990) AIAA Guidance, Navigation and Control Conference
    • Bilimoria, K.D.1    Wie, B.2
  • 9
    • 0027627810 scopus 로고
    • Singular control in minimum time spacecraft reorientation
    • July/August
    • SEYWALD, H and KUMAR, R. R. "Singular Control in Minimum Time Spacecraft Reorientation," Journal of Guidance, Control and Dynamics, Vol. 16, No. 4, July/August 1993, pp. 686-694.
    • (1993) Journal of Guidance, Control and Dynamics , vol.16 , Issue.4 , pp. 686-694
    • Seywald, H.1    Kumar, R.R.2
  • 11
    • 0030257697 scopus 로고    scopus 로고
    • Globally stable feedback laws for near-minimum-fuel and near-minimum-time pointing maneuvers for a landmark-tracking spacecraft
    • SCHAUB, H., ROBINETT, R.D., and JUNKINS, J.L. "Globally Stable Feedback Laws for Near-Minimum-Fuel and Near-Minimum-Time Pointing Maneuvers for a Landmark-Tracking Spacecraft," Journal of the Astronautical Sciences, Vol. 44, No. 4, pp. 443-466.
    • Journal of the Astronautical Sciences , vol.44 , Issue.4 , pp. 443-466
    • Schaub, H.1    Robinett, R.D.2    Junkins, J.L.3
  • 13
    • 0000781651 scopus 로고    scopus 로고
    • A globally stable linear attitude regulator
    • MORTENSEN, R. E. "A Globally Stable Linear Attitude Regulator," International Journal of Control, Vol. 8, No. 3, pp. 297-302.
    • International Journal of Control , vol.8 , Issue.3 , pp. 297-302
    • Mortensen, R.E.1
  • 16
    • 0022066858 scopus 로고    scopus 로고
    • Quaternion feedback for spacecraft large angle maneuvers
    • WIE, B. and BARBA, P. "Quaternion Feedback for Spacecraft Large Angle Maneuvers," Journal of Guidance, Control, and Dynamics, Vol. 8, No. 3, pp. 360-365.
    • Journal of Guidance, Control, and Dynamics , vol.8 , Issue.3 , pp. 360-365
    • Wie, B.1    Barba, P.2
  • 17
    • 0029410445 scopus 로고    scopus 로고
    • Feedback control logic for spacecraft eigenaxis rotations under slew rate and control constraints
    • WIE, B. and LU, J. "Feedback Control Logic for Spacecraft Eigenaxis Rotations Under Slew Rate and Control Constraints," Journal of Guidance, Control, and Dynamics, Vol. 18, No. 6, pp. 1372-1379.
    • Journal of Guidance, Control, and Dynamics , vol.18 , Issue.6 , pp. 1372-1379
    • Wie, B.1    Lu, J.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.