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15篇 您的检索式:作者名="Dukeman G"
    题名 作者 年代 出处 被引量
1Rapid optimal mul- tiburn ascent planning and guidance显示文摘Lu P Griffin B Dukeman G 2008Journal of Guid- ance Control and Dynamics2008,31,6:1
2Automatic method to compute orbital reentry trajectories with heating constraints显示文摘Zimmerman C Dukeman G Hanson J 2003Journal of Guidance Control and Dynamics2003,26,4:1
3Rapid optimal multiburn ascent planning and guidance显示文摘Lu P Griffin B Dukeman G 2008Journal of Guidance Control and Dynamics2008,31,6:1
4Automated method to compute orbital reentry trajectories with heating constraints 显示文摘Zimmerman C Dukeman G A Hanson J M 2003Journal of Guidance Control and Dynamics2003,26,4:1
5Closed-loop endo-atmospheric ascent guidance显示文摘Dukeman G A Calise A J 2003AIAA 2003-56382003,,:1
6Automatic method to com-pute orbital reentry trajectories with heating constraints显示文摘 Dukeman G and Hanson J 2003Jonrnal of Guidance Control and Dynamics2003,26,4:1
7Automatic method to compute orbital reentry trajectories with heating constraints显示文摘Zimmerman C Dukeman G and Hanson J 2003Journal of Guidance Control and Dynamics2003,26,4:1
8Automated method to compute orbital reentry trajectories with heating constraints显示文摘Zimmerman C Dukeman G Hanson J 2003Journal of Guidance Control and Dynamics2003,26,4:1
9Automatic method to compute orbital reentry trajectories with heating constraints显示文摘Zimmerman C Dukeman G Hanson J 2003Journal of Guidance Control and Dynamics2003,26,4:1
10RApiD OptiMAL MuLtiBuRN ASCENt pLANNiNg ANDguiDANCE显示文摘LU P GRIFFIN B J DUKEMAN G A Et AL 2008JOuRNAL Of GuiDANCE CONtROL ANDDyNAMiCS2008,31,6:1
11Rapid Optimal Multiburn Ascent Planning and Guidance显示文摘Lu P Griffin B Dukeman G 2008Journal of Guidance Control and Dynamics2008,31,6:1
12Atmospheric ascent guidance for rock-et-powered launch vehicles 显示文摘DUKEMAN G A 2002AIAA Paper2002,4559,:1
13An auto- mated method to compute orbital reentry trajectories with heating constraints 显示文摘ZIMMERMAN C DUKEMAN G HANSON J 2003Journal of Guidance Control and Dynamics2003,26,4:1
14Automated method to compute orbital reentry trajectories with heating constraints显示文摘Zimmerman C Dukeman G and Hanson J 2003Journal of Guidance Control and Dynamics2003,26,4:1
15Rapid optimal multiburn ascent planning and guidance显示文摘Lu Ping Griffin B J Dukeman G A Chavez F R 2008Journal of Guidance Control and Dynamics2008,31,6:1
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