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Volumn 26, Issue 2, 2003, Pages 283-294

Closed-loop endoatmospheric ascent guidance

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; BOUNDARY VALUE PROBLEMS; CLOSED LOOP CONTROL SYSTEMS; COMPUTER SIMULATION; ELECTRONIC GUIDANCE SYSTEMS; EQUATIONS OF MOTION; FINITE DIFFERENCE METHOD; LAUNCHING; OPTIMAL CONTROL SYSTEMS; REUSABLE ROCKETS;

EID: 0037348909     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.5045     Document Type: Article
Times cited : (174)

References (21)
  • 1
    • 0012689377 scopus 로고
    • General formulation of the iterative guidance mode
    • NASA TM X-53414, March
    • Smith, I. E., "General Formulation of the Iterative Guidance Mode," NASA TM X-53414, March 1966.
    • (1966)
    • Smith, I.E.1
  • 5
    • 85003342310 scopus 로고
    • Hybrid approach to near-optimal launch vehicle guidance
    • Leung, M. S. K., and Calise, A. J., "Hybrid Approach to Near-Optimal Launch Vehicle Guidance," Journal of Guidance, Control, and Dynamics, Vol. 17, No. 5, 1994, pp. 881-888.
    • (1994) Journal of Guidance, Control, and Dynamics , vol.17 , Issue.5 , pp. 881-888
    • Leung, M.S.K.1    Calise, A.J.2
  • 6
    • 0032208972 scopus 로고    scopus 로고
    • Design and evaluation of a three-dimensional optimal ascent guidance algorithm
    • Calise, A. J., Melamed, N., and Lee, S., "Design and Evaluation of a Three-Dimensional Optimal Ascent Guidance Algorithm," Journal of Guidance, Control, and Dynamics, Vol. 21, No. 6, 1998, pp. 867-875.
    • (1998) Journal of Guidance, Control, and Dynamics , vol.21 , Issue.6 , pp. 867-875
    • Calise, A.J.1    Melamed, N.2    Lee, S.3
  • 7
    • 0035280068 scopus 로고    scopus 로고
    • Optimization of launch vehicle ascent trajectories with path constraints and coast arcs
    • Gath, P. F., and Calise, A. J., "Optimization of Launch Vehicle Ascent Trajectories with Path Constraints and Coast Arcs," Journal of Guidance, Control, and Dynamics, Vol. 24, No. 2, 2001, pp. 296-304.
    • (2001) Journal of Guidance, Control, and Dynamics , vol.24 , Issue.2 , pp. 296-304
    • Gath, P.F.1    Calise, A.J.2
  • 8
    • 0003748655 scopus 로고    scopus 로고
    • HISTOS technical report 1
    • Inst. of Flight Mechanics and Control, Univ. of Stuttgart, Stuttgart, Germany, June
    • Gath, P. F., and Well, K. H., "HISTOS Technical Report 1," Inst. of Flight Mechanics and Control, Univ. of Stuttgart, Stuttgart, Germany, June 1999.
    • (1999)
    • Gath, P.F.1    Well, K.H.2
  • 9
    • 85087189620 scopus 로고    scopus 로고
    • Generation of launch vehicle abort trajectories using a hybrid optimization method
    • AIAA Paper 2002-4560, Aug.
    • Calise, A. J., and Brandt, N., "Generation of Launch Vehicle Abort Trajectories Using a Hybrid Optimization Method," AIAA Paper 2002-4560, Aug. 2002.
    • (2002)
    • Calise, A.J.1    Brandt, N.2
  • 11
    • 0012647323 scopus 로고
    • General theory of optimal trajectory for rocket flight in a resisting medium
    • Vinh, N. X., "General Theory of Optimal Trajectory for Rocket Flight in a Resisting Medium," Journal of Optimization Theory and Applications, Vol. 11, No. 2, 1973, pp. 189-202.
    • (1973) Journal of Optimization Theory and Applications , vol.11 , Issue.2 , pp. 189-202
    • Vinh, N.X.1
  • 13
    • 0031224393 scopus 로고    scopus 로고
    • Nonlinear systems with control and state constraints
    • Lu, P., "Nonlinear Systems with Control and State Constraints," Optimal Control Applications and Methods, Vol. 18, 1997, pp. 313-326.
    • (1997) Optimal Control Applications and Methods , vol.18 , pp. 313-326
    • Lu, P.1
  • 15
    • 26344469764 scopus 로고    scopus 로고
    • User's manual for DIDO 2001 (α): A MATLAB™ application package for dynamic optimization
    • Naval Postgraduate School, TR NPS-AA-01-003, Monterey, CA, Oct.
    • Ross, I. M., and Fahroo, F., "User's Manual for DIDO 2001 (α): A MATLAB™ Application Package for Dynamic Optimization," Naval Postgraduate School, TR NPS-AA-01-003, Monterey, CA, Oct. 2001.
    • (2001)
    • Ross, I.M.1    Fahroo, F.2
  • 16
    • 26344470858 scopus 로고
    • Ascent guidance for a winged boost vehicle
    • NASA CR-172083, Aug.
    • Corvin, M. A., "Ascent Guidance for a Winged Boost Vehicle," NASA CR-172083, Aug. 1988.
    • (1988)
    • Corvin, M.A.1
  • 20
    • 0004013461 scopus 로고
    • Development of a method for optimal maneuver analysis of complex space missions
    • NASA TN D-7882, April
    • McAdoo, S. F., Jezewski, D. J., and Dawkins, G. S., "Development of a Method for Optimal Maneuver Analysis of Complex Space Missions." NASA TN D-7882, April 1975.
    • (1975)
    • McAdoo, S.F.1    Jezewski, D.J.2    Dawkins, G.S.3
  • 21
    • 85085779483 scopus 로고    scopus 로고
    • Atmospheric ascent guidance for rocket-powered launch vehicles
    • AIAA Paper 2002-4559, Aug.
    • Dukeman, G. A., "Atmospheric Ascent Guidance for Rocket-Powered Launch Vehicles," AIAA Paper 2002-4559, Aug. 2002.
    • (2002)
    • Dukeman, G.A.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.