Optimum Non-dimensional Thrust for the Minimum Fuel Trajectory of a Lunar Lander
Author:
Affiliation:
1. 連絡先著者（Corresponding author）：ueno-seiya-wk@ynu.ac.jp
2. 横浜国立大学大学院環境情報研究院
Publisher
Japan Society for Aeronautical and Space Sciences
Subject
General Medicine
Link
https://www.jstage.jst.go.jp/article/jjsass/70/4/70_70_105/_pdf
Reference5 articles.
1. 1) Bennett, F. V.: Apollo Experience Report Mission Planning for Lunar Module Descent and Ascent, NASA TN D-6846, 1972.
2. 2) Ramanan, R. V. and Lai, M.: Analysis of Optimal Strategies for Soft Landing on the Moon from a Parking Orbits, J. Earth Syst. Sci., 114, 6 (2005), pp. 807-813.
3. 3) Park, B.-G., Ahn, J.-S. and Tahk, M.-J.: Two-Dimensional Trajectory Optimization for Soft Lunar Landing Considering a Landing Site, Int. J. Aeronaut. Space Sci., 12, 3 (2011), pp. 288-295.
4. 4) Cho, D.-H., Kim, D. and Leeghim, H.: Optimal Lunar Landing Trajectory Design for Hybrid Engines, Mathematical Problems in Engineering, 2015 (2015), Article ID 462072.
5. 5) Zhu, L., Ma, J. and Wang, S.: Deep Neural Networks Based Real-time Optimal Control for Lunar Lander, IOP Conference Series: Materials and Engineering, 608 (2019), doi: 10.1088/1757-899X/608/1/012045.
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