Computative Analysis of Re-entry Vehicle and Calculation of the Shortest Power Landing Distance Within Martian Airspace
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-19-6945-4_67
Reference10 articles.
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3. Blackmore L, Açikmeşe B, Scharf DP (2012) Minimum-landing-error powered-descent guidance for Mars landing using convex optimization. 33(4):1161–1171, May 2012. https://doi.org/10.2514/1.47202
4. Meditch JS (1964) On the problem of optimal thrust programming for a lunar soft landing. IEEE Trans Automat Contr 9(4):477–484. https://doi.org/10.1109/TAC.1964.1105758
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