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Mathematical Problems in Engineering
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Special Issues
Mathematical Problems in Engineering
/
2017
/
Article
/
Tab 1
/
Research Article
Adaptive Mesh Iteration Method for Trajectory Optimization Based on Hermite-Pseudospectral Direct Transcription
Table 1
Hypersonic boost-glide vehicle date and physical constants.
Quantity
Numerical values
Mass (kg)
1200
(kg/m
2
)
420
(m)
(kg/m
3
)
(m
2
/s
2
)
(m)