Optimisation of the Terminal Flight Phase for a Future Reusable Launch Vehicle
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[1] M. H. Gräßlin,et al. Ascent and reentry guidance concept based on NLP-methods , 2004 .
[2] Michael Ruth,et al. Aerodynamic characteristics, database development and flight simulation of the X-34 vehicle , 2000 .
[3] J. W. Kraemer,et al. Shuttle orbiter guidance system for the terminal flight phase , 1977, Autom..