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Volumn 19, Issue 9, 2005, Pages 1695-1705

Time optimal attitude maneuver strategies for the agile spacecraft with reaction wheels and thrusters

Author keywords

Hybrid Control; Reaction Wheel; Thrusting Logics; Time Optimal Control

Indexed keywords


EID: 30344485990     PISSN: 1738494X     EISSN: None     Source Type: Journal    
DOI: 10.1007/BF02984181     Document Type: Article
Times cited : (13)

References (15)
  • 1
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    • Time optimal three-axis reorientation of a rigid spacecraft
    • Bilimoria, K. D. and Wie, B., 1993, "Time Optimal Three-Axis Reorientation of a Rigid Spacecraft," Journal of Guidance, Control, and Dynamics, vol. 16, no. 3, pp. 446-452.
    • (1993) Journal of Guidance, Control, and Dynamics , vol.16 , Issue.3 , pp. 446-452
    • Bilimoria, K.D.1    Wie, B.2
  • 2
    • 0027593213 scopus 로고
    • Quasi-closed-form solution to the time-optimal rigid spacecraft reorientation problem
    • Byers, R. M. and Vadali, S. R., 1993, "Quasi-Closed-Form Solution to the Time-Optimal Rigid Spacecraft Reorientation Problem," Journal of Guidance, Control and Dynamics, vol. 16, no. 3, pp. 453-461.
    • (1993) Journal of Guidance, Control and Dynamics , vol.16 , Issue.3 , pp. 453-461
    • Byers, R.M.1    Vadali, S.R.2
  • 4
    • 85039345973 scopus 로고    scopus 로고
    • "Varying Time Division Pulsing Method and its Controller for Coupled Thrusting Satellite," Patent Pending in Korea
    • KARI and HAU, 2003, "Varying Time Division Pulsing Method and its Controller for Coupled Thrusting Satellite," Patent Pending in Korea.
    • (2003)
    • Kari1    Hau2
  • 6
    • 0027685324 scopus 로고
    • A survey of attitude representations
    • Malcolm, D. S., 1993, "A Survey of Attitude Representations," Journal of the Astronautical Sciences, vol. 41, no. 4, pp. 439-517.
    • (1993) Journal of the Astronautical Sciences , vol.41 , Issue.4 , pp. 439-517
    • Malcolm, D.S.1
  • 7
    • 30344480194 scopus 로고    scopus 로고
    • Attitude control by asymmetric thrusters' independent off modulation during orbit adjustment maneuvers
    • Oh, H. S., 1999, "Attitude Control by Asymmetric Thrusters' Independent Off Modulation During Orbit Adjustment Maneuvers," Journal of Astronomy and Space Sciences in Korea, vol. 16, no. 2, pp. 265-212.
    • (1999) Journal of Astronomy and Space Sciences in Korea , vol.16 , Issue.2 , pp. 265-1212
    • Oh, H.S.1
  • 8
    • 30344471796 scopus 로고    scopus 로고
    • Minimum fuel back-up attitude control and momentum dumping of a satellite with an asymmetric thruster configuration
    • Oh, H. S. and Hwang, J. H., 1999, "Minimum Fuel Back-Up Attitude Control and Momentum Dumping of a Satellite with an Asymmetric Thruster Configuration," Journal of Korean Society for Aeronautical and Space Sciences in Korea, vol. 27, no. 6, pp. 105-115.
    • (1999) Journal of Korean Society for Aeronautical and Space Sciences in Korea , vol.27 , Issue.6 , pp. 105-115
    • Oh, H.S.1    Hwang, J.H.2
  • 9
    • 0035374299 scopus 로고    scopus 로고
    • Torque and force measurement of a prototype HAU reaction wheel and the effect of disturbance on the attitude stability of spacecraft
    • Oh, H. S., Kwon, J. W., Lee, H., Nam, M. R. and Park, D. J., 2001, "Torque and Force Measurement of a Prototype HAU Reaction Wheel and the Effect of Disturbance on the Attitude Stability of spacecraft," KSME International Journal, vol. 15, no. 6, pp. 743-751.
    • (2001) KSME International Journal , vol.15 , Issue.6 , pp. 743-751
    • Oh, H.S.1    Kwon, J.W.2    Lee, H.3    Nam, M.R.4    Park, D.J.5
  • 10
    • 17044407159 scopus 로고    scopus 로고
    • Precision measurements of reaction wheel disturbances with frequency compensation process
    • Oh, H. S. and Cheon, D. I., 2005, "Precision Measurements of Reaction Wheel Disturbances with Frequency Compensation Process," Journal of Mechanical Science and Technology, KSME, vol. 19, no. 1, pp. 136-143.
    • (2005) Journal of Mechanical Science and Technology, KSME , vol.19 , Issue.1 , pp. 136-143
    • Oh, H.S.1    Cheon, D.I.2
  • 11
    • 0027720887 scopus 로고
    • Time optimal reorientation of a rigid spacecraft using collocation and nonlinear programming
    • Scrivener, S. L. and Thomson, R. C., 1993, "Time Optimal Reorientation of a Rigid Spacecraft using Collocation and nonlinear Programming," Advances in the Astronautical Sciences, vol. 85, no. 3, pp. 1905-1924.
    • (1993) Advances in the Astronautical Sciences , vol.85 , Issue.3 , pp. 1905-1924
    • Scrivener, S.L.1    Thomson, R.C.2
  • 12
    • 0027627810 scopus 로고
    • Singular control in minimum time spacecraft reorientation
    • Seywald, H. and Kumar, R. R., 1993, "Singular Control in Minimum Time Spacecraft Reorientation," Journal of Guidance, Control and Dynamics, vol. 16, no. 4, pp. 686-694.
    • (1993) Journal of Guidance, Control and Dynamics , vol.16 , Issue.4 , pp. 686-694
    • Seywald, H.1    Kumar, R.R.2
  • 13
    • 0001687520 scopus 로고    scopus 로고
    • Time-optimal control of axi-symmetric rigid spacecraft using two controls
    • Shen, H. and Tsiotras, P., 1999, "Time-Optimal Control of Axi-symmetric Rigid Spacecraft Using Two Controls," Journal of Guidance, Control, and Dynamics, vol. 22, no. 5, pp. 682-694.
    • (1999) Journal of Guidance, Control, and Dynamics , vol.22 , Issue.5 , pp. 682-694
    • Shen, H.1    Tsiotras, P.2
  • 15
    • 0029368453 scopus 로고
    • Near-minimum-time eigenaxis rotation maneuvers using reaction wheels
    • Steyn, W. H., 1995, "Near-Minimum-Time Eigenaxis Rotation Maneuvers Using Reaction Wheels," Journal of Guidance, Control and Dynamics, vol. 18, no. 5, pp. 446-452.
    • (1995) Journal of Guidance, Control and Dynamics , vol.18 , Issue.5 , pp. 446-452
    • Steyn, W.H.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.