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Volumn 22, Issue 5, 1999, Pages 625-631

Optimal Aeroassisted Orbital Interception

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EID: 0000316703     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4435     Document Type: Article
Times cited : (20)

References (18)
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    • Hargraves, C.R.1    Paris, S.W.2
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    • Optimal Finite-Thrust Spacecraft Trajectories Using Collocation and Nonlinear Programming
    • Enright, P. J., and Conway, B. A., "Optimal Finite-Thrust Spacecraft Trajectories Using Collocation and Nonlinear Programming," Journal of Guidance, Control, and Dynamics, Vol. 14, No. 5, 1991, pp. 981-985.
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    • Enright, P.J.1    Conway, B.A.2
  • 5
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    • Direct Optimization Using Collocation Based on High-Order Gauss-Lobatto Quadrature Rules
    • Herman, A. L., and Conway, B. A., "Direct Optimization Using Collocation Based on High-Order Gauss-Lobatto Quadrature Rules," Journal of Guidance, Control, and Dynamics, Vol. 19, No. 3, 1996, pp. 592-599.
    • (1996) Journal of Guidance, Control, and Dynamics , vol.19 , Issue.3 , pp. 592-599
    • Herman, A.L.1    Conway, B.A.2
  • 6
    • 0022733451 scopus 로고
    • Optimal Trajectory for Aeroassisted Noncoplanar Orbital Transfer
    • Miele, A., Basapur, V. K., and Lee, W. Y., "Optimal Trajectory for Aeroassisted Noncoplanar Orbital Transfer," Acta Astronautica, Vol. 15, No. 6/7, 1987, pp. 399-411.
    • (1987) Acta Astronautica , vol.15 , Issue.6-7 , pp. 399-411
    • Miele, A.1    Basapur, V.K.2    Lee, W.Y.3
  • 7
    • 0030134945 scopus 로고    scopus 로고
    • Recent Advances in the Optimization and Guidance of Aeroassisted Orbital Transfers
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    • Miele, A.1
  • 8
    • 0040473644 scopus 로고
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    • Medepalli, S., and Vinh, N. X., "Optimal Plane Change of an Elliptic Orbit During Aerocruise," Journal of Astronautical Sciences, Vol. 40, No. 4, 1992, pp. 503-525.
    • (1992) Journal of Astronautical Sciences , vol.40 , Issue.4 , pp. 503-525
    • Medepalli, S.1    Vinh, N.X.2
  • 10
    • 0030150499 scopus 로고    scopus 로고
    • Variational Solution for the Heat-Rate-Limited Aeroassisted Orbital Transfer Problem
    • Seywald, H., "Variational Solution for the Heat-Rate-Limited Aeroassisted Orbital Transfer Problem," Journal of Guidance, Control, and Dynamics, Vol. 19, No. 3, 1996, pp. 686-692.
    • (1996) Journal of Guidance, Control, and Dynamics , vol.19 , Issue.3 , pp. 686-692
    • Seywald, H.1
  • 11
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    • Maximum Orbit Plane Change with Heat-Transfer-Rate Considerations
    • Lee, J. Y., and Hull, D. G., "Maximum Orbit Plane Change with Heat-Transfer-Rate Considerations," Journal of Guidance, Control, and Dynamics, Vol. 13, No. 3, 1990, pp. 492-497.
    • (1990) Journal of Guidance, Control, and Dynamics , vol.13 , Issue.3 , pp. 492-497
    • Lee, J.Y.1    Hull, D.G.2
  • 17
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    • Benefits of High Aerodynamic Efficiency to Orbital Transfer Vehicles
    • Aug.
    • Andrews, D. G., Norris, R. B., and Paris, S. W., "Benefits of High Aerodynamic Efficiency to Orbital Transfer Vehicles," AIAA Paper 83-2109, Aug. 1983.
    • (1983) AIAA Paper 83-2109
    • Andrews, D.G.1    Norris, R.B.2    Paris, S.W.3
  • 18
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    • Aeroassisted Orbital Transfer Trajectory Optimization Using Direct Methods
    • Aug.
    • Zimmermann, F., and Calise, A. J., "Aeroassisted Orbital Transfer Trajectory Optimization Using Direct Methods," AIAA Paper 95-3478, Aug. 1995.
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.