Feasibility Analysis of Hypersonic Vehicles Trajectory Under Multiple Constraints
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Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-19-6613-2_548
Reference16 articles.
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3. Dalle, D., Torrez, S., Driscoll, J.: Minimum-fuel ascent of a hypersonic vehicle using surrogate optimization. J. Aircr. 51(6), 1973–1986 (2014)
4. Pescetelli, F., Minisci, E., Maddock, C.: Ascent trajectory optimisation for a single-stage-to-orbit vehicle with hybrid propulsion. In: AIAA 18th International Space Planes Hypersonic Systems and Technologies Conference, Tours, France, pp. 1–18 (2012)
5. Chudej, K., Bulirsch, R.: Numerical solution of a simultaneous staging and trajectory optimization problem of a hypersonic space vehicle. In: AIAA/DGLR 5th International Aerospace Planes and Hypersonics Technologies Conference, Munich, Germany, pp. 1–10 (1993)
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