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Volumn 52, Issue 4, 2004, Pages 517-530

Adaptive dynamic inversion control with actuator saturation constraints applied to tracking spacecraft maneuvers

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE PARAMETERS; INVERSION CONTROL; PERSISTANT EXCITATION; RIGID SPACECRAFT; ACTUATOR SATURATIONS; ASYMPTOTIC CONVERGENCE; ASYMPTOTIC TRACKING; CONTROL SATURATION; PERSISTENT EXCITATION; REFERENCE TRAJECTORIES; SPACECRAFT MANEUVERS;

EID: 27744581260     PISSN: 00219142     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article
Times cited : (35)

References (24)
  • 4
    • 0034308470 scopus 로고    scopus 로고
    • Adaptive realization of linear closed-loop tracking dynamics in the presence of large system model errors
    • Oct.-Dec.
    • SCHAUB, H., AKELLA, M. R., and JUNKINS, J. L. "Adaptive Realization of Linear Closed-Loop Tracking Dynamics in the Presence of Large System Model Errors," The Journal of Astronautical Sciences, Vol 48, No. 4. Oct.-Dec. 2000. pp 537-551.
    • (2000) The Journal of Astronautical Sciences , vol.48 , Issue.4 , pp. 537-551
    • Schaub, H.1    Akella, M.R.2    Junkins, J.L.3
  • 9
    • 85087599272 scopus 로고    scopus 로고
    • Structured adaptive model inversion applied to tracking aggressive aircraft maneuvers
    • presented as paper AIAA 2001-4019 Montreal, Canada, August 6-9
    • SUBBARAO, K., STEINBERG, M., and JUNKINS, J.L. "Structured Adaptive Model Inversion Applied to Tracking Aggressive Aircraft Maneuvers," presented as paper AIAA 2001-4019 at the AIAA Guidance, Navigation, and Control Conference, Montreal, Canada, August 6-9, 2001.
    • (2001) AIAA Guidance, Navigation, and Control Conference
    • Subbarao, K.1    Steinberg, M.2    Junkins, J.L.3
  • 10
    • 85086494651 scopus 로고    scopus 로고
    • Fault tolerant structured adaptive model inversion
    • presented as paper AIAA 2003-0015 Reno, NV, January 6-9
    • TANDALE, M. D. "Fault Tolerant Structured Adaptive Model Inversion," presented as paper AIAA 2003-0015 at the AIAA Aerospace Sciences Conferences and Exhibit, Reno, NV, January 6-9, 2003.
    • (2003) AIAA Aerospace Sciences Conferences and Exhibit
    • Tandale, M.D.1
  • 11
    • 84896693851 scopus 로고    scopus 로고
    • Structured adaptive model inversion control to simultaneously handle actuator failure and actuator saturation
    • presented as paper AIAA 2003-5325 Austin, TX, August 11-14
    • TANDALE, M. D. and VALASEK, J. "Structured Adaptive Model Inversion Control to Simultaneously Handle Actuator Failure and Actuator Saturation," presented as paper AIAA 2003-5325 at the AIAA Guidance Navigation and Control Conference and Exhibit, Austin, TX, August 11-14, 2003.
    • (2003) AIAA Guidance Navigation and Control Conference and Exhibit
    • Tandale, M.D.1    Valasek, J.2
  • 13
    • 0030243148 scopus 로고    scopus 로고
    • Nonlinear small gain theorem for the analysis of control systems with saturation
    • September
    • TEEL, A. R. "Nonlinear Small Gain Theorem for the Analysis of Control Systems with Saturation," IEEE Transactions on Automatic Control, Vol. 21, No. 9, September, 1996, pp. 1256-1270.
    • (1996) IEEE Transactions on Automatic Control , vol.21 , Issue.9 , pp. 1256-1270
    • Teel, A.R.1
  • 16
    • 84983134257 scopus 로고    scopus 로고
    • Structured model reference adaptive control with actuator saturation limits
    • presented as paper AIAA 1998-4472 Boston, MA, August 10-12
    • AKELLA, M. R. and JUNKINS, J. L. "Structured Model Reference Adaptive Control with Actuator Saturation Limits," presented as paper AIAA 1998-4472 at the AIAA/AAS Astrodynamics Specialist Conference and Exhibit, Boston, MA, August 10-12, 1998.
    • (1998) AIAA/AAS Astrodynamics Specialist Conference and Exhibit
    • Akella, M.R.1    Junkins, J.L.2
  • 17
    • 0003476209 scopus 로고    scopus 로고
    • Ph.D. dissertation, School of Aerospace Engineering, Georgia Institute of Technology
    • JOHNSON, E. "Limited Authority Adaptive Flight Control," Ph.D. dissertation, School of Aerospace Engineering, Georgia Institute of Technology, 2000.
    • (2000) Limited Authority Adaptive Flight Control
    • Johnson, E.1
  • 18
    • 85085777346 scopus 로고    scopus 로고
    • A six degree of freedom adaptive flight control architecture for trajectory following
    • presented as paper AIAA 2002-4776, Monterey, California, 5-8 August
    • JOHNSON, E. N., CALISE, A. J., and CORBAN, J.E. "A Six Degree of Freedom Adaptive Flight Control Architecture for Trajectory Following," presented as paper AIAA 2002-4776, AIAA Guidance Navigation and Control Conference and Exhibit, Monterey, California, 5-8 August 2002.
    • (2002) AIAA Guidance Navigation and Control Conference and Exhibit
    • Johnson, E.N.1    Calise, A.J.2    Corban, J.E.3
  • 19
    • 85078724392 scopus 로고    scopus 로고
    • Adaptive flight control for an autonomous unmanned helicopter
    • presented as paper AIAA 2002-4776 Monterey, California, 5-8 August
    • JOHNSON, E.N. and KANNAN, S. K. "Adaptive Flight Control for an Autonomous Unmanned Helicopter," presented as paper AIAA 2002-4776 at the AIAA Guidance Navigation and Control Conference and Exhibit, Monterey, California, 5-8 August 2002.
    • (2002) AIAA Guidance Navigation and Control Conference and Exhibit
    • Johnson, E.N.1    Kannan, S.K.2
  • 20
    • 0344898942 scopus 로고    scopus 로고
    • Limited authority adaptive flight control for reusable launch vehicles
    • JOHNSON, E. N. and CALISE, A. J. "Limited Authority Adaptive Flight Control for Reusable Launch Vehicles," AIAA Journal of Guidance, Control and Dynamics, 2003, Vol. 26, No. 6, pp. 906-913.
    • (2003) AIAA Journal of Guidance, Control and Dynamics , vol.26 , Issue.6 , pp. 906-913
    • Johnson, E.N.1    Calise, A.J.2
  • 21
    • 0032165657 scopus 로고    scopus 로고
    • Adaptive asymptotic tracking of spacecraft attitude motion with inertia matrix identification
    • Sept.-Oct.
    • AHMED, J., COPPOLA, V.T., and BERNSTEIN, D.S. "Adaptive Asymptotic Tracking of Spacecraft Attitude Motion with Inertia Matrix Identification," AIAA Journal of Guidance, Control and Dynamics, Vol. 21, No. 5, Sept.-Oct. 1998, pp. 684-691.
    • (1998) AIAA Journal of Guidance, Control and Dynamics , vol.21 , Issue.5 , pp. 684-691
    • Ahmed, J.1    Coppola, V.T.2    Bernstein, D.S.3
  • 23
    • 0033284458 scopus 로고    scopus 로고
    • Adaptive control of nonlinear attitude motions realizing linear closed-loop dynamics
    • San Diego, California, June
    • SCHAUB, H., AKELLA, M. R., and JUNKINS, J. L. "Adaptive Control of Nonlinear Attitude Motions Realizing Linear Closed-Loop Dynamics," Proceedings of the American Control Conference, Vol. 3, San Diego, California, June, 1999, pp. 1563-1567.
    • (1999) Proceedings of the American Control Conference , vol.3 , pp. 1563-1567
    • Schaub, H.1    Akella, M.R.2    Junkins, J.L.3
  • 24
    • 8744244045 scopus 로고    scopus 로고
    • Structured adaptive model inversion control with actuator saturation constraints applied to tracking spacecraft maneuvers
    • Boston, MA, June 30-July 2
    • TANDALE, M.D., SUBBARAO, K., VALASEK, J., and AKELLA, M. R. "Structured Adaptive Model Inversion Control with Actuator Saturation Constraints Applied to Tracking Spacecraft Maneuvers," Proceedings of the American Control Conference, Vol. 2, Boston, MA, June 30-July 2, 2004, pp. 1031-1036.
    • (2004) Proceedings of the American Control Conference , vol.2 , pp. 1031-1036
    • Tandale, M.D.1    Subbarao, K.2    Valasek, J.3    Akella, M.R.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.