Abstract
The periodic skip-glide trajectory models for hypersonic vehicle in near space were brought out and simulated in this paper. Firstly, the basic concepts of hypersonic vehicle and different trajectory modes were introduced in detail. Then, the three degrees of freedom model of hypersonic vehicle was given. Lastly, the model was simulated and analyzed using MATLAB. The difference changing trend of periodic trajectory, velocity, effective range, trajectory obliquity and dynamic pressure are given. How the main factors such as trajectory obliquity, launch orientation affect the periodicity was also studied. The primary simulations show that the periodic trajectory of hypersonic vehicle helpful in studying new space vehicle.
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© 2012 Springer-Verlag Berlin Heidelberg
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Shi, Z., Zhou, D., Wang, S., Pan, L. (2012). Simulation of Skip-Glide Trajectory for Hypersonic Vehicle in Near Space. In: Xiao, T., Zhang, L., Ma, S. (eds) System Simulation and Scientific Computing. ICSC 2012. Communications in Computer and Information Science, vol 326. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-34381-0_29
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DOI: https://doi.org/10.1007/978-3-642-34381-0_29
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-34380-3
Online ISBN: 978-3-642-34381-0
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