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Volumn , Issue , 1996, Pages 1-11

Nonlinear drag-tracking control applied to optimal low-lift reentry guidance

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL SYSTEMS; CONTROL THEORY; ELECTRONIC GUIDANCE SYSTEMS; FEEDBACK LINEARIZATION; LINEAR CONTROL SYSTEMS; NAVIGATION;

EID: 84959128954     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (13)

References (24)
  • 1
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    • Schöttle, U.1
  • 3
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    • Rept No. ACRV-A-TN 1.2.2, Aerospatiale, France
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  • 4
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  • 5
    • 0027662587 scopus 로고
    • Six-Degree-of-Freedom Guidance and Control-Entry Analysis of the HL-20
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    • (1993) J. of Spacecraft and Rockets , vol.30 , Issue.5 , pp. 537-542
    • Powell, R.W.1
  • 6
    • 0027657648 scopus 로고
    • Trajectory Control for a Low-Lift Re-Entry Vehicle
    • Roenneke, A. J., and Cornwell, P. J. ‘Trajectory Control for a Low-Lift Re-Entry Vehicle,” J. of Guidance, Control and Dynamics,Vol. 16, No. 5,1993, pp. 927-933.
    • (1993) J. of Guidance, Control and Dynamics , vol.16 , Issue.5 , pp. 927-933
    • Roenneke, A.J.1    Cornwell, P.J.2
  • 7
    • 85003301415 scopus 로고
    • Re-Entry Control to a Drag-vs-Energy Profile
    • Roenneke, A. J., and Markl, A. “Re-Entry Control to a Drag-vs-Energy Profile,”J, of Guidance, Control and Dynamics, Vol. 17, No. 5,1994, pp. 916-920.
    • (1994) J, of Guidance, Control and Dynamics , vol.17 , Issue.5 , pp. 916-920
    • Roenneke, A.J.1    Markl, A.2
  • 8
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    • Rept No. CR 9359- 91-NL-JG, Noordwijk, Netherlands
    • ACRI and Laboratoire d’Automatique de Nantes. Guidance and Control for Moderate Lift/Drag Re-Entry, European Space Research and Technology Center, Rept No. CR 9359- 91-NL-JG, Noordwijk, Netherlands, 1992.
    • (1992) European Space Research and Technology Center
  • 9
    • 84959172233 scopus 로고
    • NLP Re-Entry Guidance: Developing a Strategy for Low L/D Vehicles
    • Cramer, E. J., Bradt, J. E., and Hardtla, J. W. “NLP Re-Entry Guidance: Developing a Strategy for Low L/D Vehicles,” J. of Guidance, Control and Dynamics, Vol. 14, No. 6, 1991, pp. 1181-1190.
    • (1991) J. of Guidance, Control and Dynamics , vol.14 , Issue.6 , pp. 1181-1190
    • Cramer, E.J.1    Bradt, J.E.2    Hardtla, J.W.3
  • 10
    • 84959160947 scopus 로고
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  • 14
    • 84959097129 scopus 로고    scopus 로고
    • Guidance Algorithm for Suborbital Flight Experiment of Unmanned Lifiting Reentry Vehicle
    • (Baltimore, Md.), AIAA, Washington, D.C., AIAA 95-3286- CR1995
    • Ishimoto, S. “Guidance Algorithm for Suborbital Flight Experiment of Unmanned Lifiting Reentry Vehicle,” Proc. of 1995. MM. Conf. on Guidance, Navigation and Control (Baltimore, Md.), AIAA, Washington, D.C., AIAA 95-3286- CR1995, pp. 1046-1053.
    • Proc. of 1995. MM. Conf. on Guidance, Navigation and Control , pp. 1046-1053
    • Ishimoto, S.1
  • 15
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    • Küpper, X, and Chen, L. “Bin Konzept für den automatisierten Landeanflug und die automatisierte Landung von Raumfähren unter Verwendung eines inversen Modells,” Proc. of 1988. DGLR Jahrestagung (Darmstadt, Germany), Paper No. 88-086, DGLR, Bonn, Germany, 1988, pp. 1010-1018.
    • (1988) Proc. of 1988. DGLR Jahrestagung , pp. 1010-1018
    • Küpper, X.1    Chen, L.2
  • 16
    • 0028550587 scopus 로고
    • Shuttle Entry Guidance Revisited Using Nonlinear Geometric Methods
    • Mease, K. D., and Kremer, J. P. “Shuttle Entry Guidance Revisited Using Nonlinear Geometric Methods,” J. of Guidance, Control and Dynamics, Vol.17, No. 6, 1994, pp. 1350-1356.
    • (1994) J. of Guidance, Control and Dynamics , vol.17 , Issue.6 , pp. 1350-1356
    • Mease, K.D.1    Kremer, J.P.2
  • 18
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    • ALTOS Reentry Applications Manual
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    • Roenneke, A. J. ALTOS Reentry Applications Manual, Advanced Launch and Reentry Trajectory Optimization Software (ALTOS), Rept. No. ALTOS TR 96-02, InsL of Flight Mechanis and Control, University of Stuttgart, Germany, My 1996.
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  • 19
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  • 22
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.