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Volumn 18, Issue 3, 1995, Pages 561-566

Approximate altitude transitions for high-speed aircraft

Author keywords

[No Author keywords available]

Indexed keywords


EID: 85003354987     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.21423     Document Type: Article
Times cited : (14)

References (15)
  • 1
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    • Petersen, R. H., Gregory, T. J., and Smith C. L., “Some Comparisons of Turboramjet-Powered Hypersonic Aircraft for Cruise and Boost Missions,” Journal of Aircraft, Vol. 3, No. 5, 1966, p. 398.
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    • Petersen, R.H.1    Gregory, T.J.2    Smith, C.L.3
  • 3
    • 84999107930 scopus 로고
    • Optimal Trajectories for Hypersonic Launch Vehicles
    • edited by J. M. Skowronski, H. Flashner, and R. S. Guttalu, Springer-Verlag, Berlin
    • Ardema, M. D., Bowles, J. V., and Whittaker, T., “Optimal Trajectories for Hypersonic Launch Vehicles,” Lecture Notes in Control and Information Sciences, Vol. 170, edited by J. M. Skowronski, H. Flashner, and R. S. Guttalu, Springer-Verlag, Berlin, 1992, p. 18.
    • (1992) Lecture Notes in Control and Information Sciences , vol.170 , pp. 18
    • Ardema, M.D.1    Bowles, J.V.2    Whittaker, T.3
  • 4
    • 0014604030 scopus 로고
    • Energy-State Approximation in Performance Optimization of Supersonic Aircraft
    • Bryson, A. E., Jr., Desai, M. N., and Hoffman, W. C., “Energy-State Approximation in Performance Optimization of Supersonic Aircraft,” Journal of Aircraft, Vol. 6, No. 6, 1969, p. 481.
    • (1969) Journal of Aircraft , vol.6 , Issue.6 , pp. 481
    • Bryson, A.E.1    Desai, M.N.2    Hoffman, W.C.3
  • 6
    • 0016973115 scopus 로고
    • Solution of Minimum Time-to-Climb Problem by Matched Asymptotic Expansions
    • Ardema, M. D., “Solution of Minimum Time-to-Climb Problem by Matched Asymptotic Expansions,” AIAA Journal, Vol. 14, No. 7, 1976, p. 843.
    • (1976) AIAA Journal , vol.14 , Issue.7 , pp. 843
    • Ardema, M.D.1
  • 7
    • 85012702422 scopus 로고
    • Aircraft Maneuver Optimization by Reduced-Order Approximation
    • edited by C. T. Leondes, Academic, New York
    • Kelley, H. J., “Aircraft Maneuver Optimization by Reduced-Order Approximation,” Control and Dynamic Systems, Vol. 10, edited by C. T. Leondes, Academic, New York, 1973, p. 131.
    • (1973) Control and Dynamic Systems , vol.10 , pp. 131
    • Kelley, H.J.1
  • 9
    • 0026257295 scopus 로고
    • Rapid Near-Optimal Aerospace Plane Trajectory Generation and Guidance
    • Corban, J. E., Calise, A. J., and Flandro, G. A.,“Rapid Near-Optimal Aerospace Plane Trajectory Generation and Guidance,” Journal of Guidance, Control, andDynamics, Vol. 14, No. 6, 1991, p. 1181.
    • (1991) Journal of Guidance, Control, Anddynamics , vol.14 , Issue.6 , pp. 1181
    • Corban, J.E.1    Calise, A.J.2    Flandro, G.A.3
  • 10
    • 0017521869 scopus 로고
    • Optimal Flight-Path- Angle Transitions in MinimumTime Airplane Climbs
    • Breakwell, J. V., “Optimal Flight-Path- Angle Transitions in MinimumTime Airplane Climbs,” Journal of Aircraft, Vol. 14, No. 8, 1977, p. 782.
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    • Breakwell, J.V.1
  • 11
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    • More About Flight-Path-Angle Transitions in Optimal Airplane Climbs
    • Breakwell, J. V., “More About Flight-Path-Angle Transitions in Optimal Airplane Climbs,” Journal of Guidance and Control, Vol. 1, No. 3, 1978, p. 205.
    • (1978) Journal of Guidance and Control , vol.1 , Issue.3 , pp. 205
    • Breakwell, J.V.1
  • 12
    • 0020721246 scopus 로고
    • Altitude Transitions in Energy Climbs
    • Weston, A. R., Cliff, E. M., and Kelley, H. J., “Altitude Transitions in Energy Climbs,” Automatica, Vol. 19, No. 2, 1983, p. 199.
    • (1983) Automatica , vol.19 , Issue.2 , pp. 199
    • Weston, A.R.1    Cliff, E.M.2    Kelley, H.J.3
  • 13
    • 0023849251 scopus 로고
    • Interior Transition Layers in Flight-Path Optimization
    • Ardema, M. D., and Yang, L., “Interior Transition Layers in Flight-Path Optimization,” Journal of Guidance, Control, and Dynamics, Vol. 11, No. 1, 1988, p. 13.
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    • Ardema, M.D.1    Yang, L.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.