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Volumn , Issue , 1996, Pages 1-11

Heat input reduction in hypersonic flight by optimal trajectory control

Author keywords

[No Author keywords available]

Indexed keywords

EQUATIONS OF MOTION; FLIGHT PATHS; HEAT TRANSFER;

EID: 84959093883     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-3905     Document Type: Conference Paper
Times cited : (3)

References (16)
  • 2
    • 85003368800 scopus 로고
    • Thermostructural Concepts for Hypervelocity Vehicles
    • P. K. Shih, J. Prunty, and R. N. Mueller. Thermostructural Concepts for Hypervelocity Vehicles. Journal of Aircraft, 28(5):337-345, May 1991.
    • (1991) Journal of Aircraft , vol.28 , Issue.5 , pp. 337-345
    • Shih, P.K.1    Prunty, J.2    Mueller, R.N.3
  • 5
    • 0242435751 scopus 로고
    • Combined Optimization of Trajectory and Stage Separation of a Hypersonic Two-Stage Space Vehicle
    • R. Bulirsch and K. Chudej. Combined Optimization of Trajectory and Stage Separation of a Hypersonic Two-Stage Space Vehicle. Zeitschrift für Flugvnssenschaften und Weltraumforschung, 19(1):55-60, 1995.
    • (1995) Zeitschrift für Flugvnssenschaften Und Weltraumforschung , vol.19 , Issue.1 , pp. 55-60
    • Bulirsch, R.1    Chudej, K.2
  • 8
    • 84959104211 scopus 로고
    • Trajectory Optimization and Guidance for a Hermes-Type Reentry Vehicle
    • C. Jänsch and A. Markl. Trajectory Optimization and Guidance for a Hermes-Type Reentry Vehicle. In AIAA-91-2659, 1991.
    • (1991) AIAA-91-2659
    • Jänsch, C.1    Markl, A.2
  • 14
    • 84894498924 scopus 로고
    • Flight Trajectory Control for Thermal Abatement of Hypersonic Vehicles
    • Orlando, October
    • J. R. Ring. Flight Trajectory Control for Thermal Abatement of Hypersonic Vehicles. In AIAA Snd International Aerospace Planes Conference, Orlando, October 1990.
    • (1990) AIAA Snd International Aerospace Planes Conference
    • Ring, J.R.1
  • 15
    • 84976243679 scopus 로고
    • Stability Analysis of Atmospheric Trajectory of Space Plane for Dynamic Pressure/Heat-Input Rate Control
    • K. Yonemoto, T. Mugitani, and T. Makino. Stability Analysis of Atmospheric Trajectory of Space Plane for Dynamic Pressure/Heat-Input Rate Control. In DGLR Jahrbuch 7, pp. 503-511, 1989.
    • (1989) DGLR Jahrbuch , vol.7 , pp. 503-511
    • Yonemoto, K.1    Mugitani, T.2    Makino, T.3
  • 16
    • 8644228273 scopus 로고
    • Institut fur Robotik und Systemdynamik, DLR, Oberpfaffenhofen
    • GESOP (Graphical Environment for Simulation and Optimization), Softwaresystem für die Bahnoptimierung. Institut fur Robotik und Systemdynamik, DLR, Oberpfaffenhofen, 1993.
    • (1993) Softwaresystem für Die Bahnoptimierung


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.