Gotowe bibliografie tematyczne / Lunar Soft-Landing

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  1. Artykuły w czasopismach
  2. Rozprawy doktorskie
  3. Książki
  4. Części książek
  5. Streszczenia konferencji

Gotowa bibliografia na temat „Lunar Soft-Landing”

Autor: Grafiati
Data publikacji: 6 września 2023
Data aktualizacji: 31 lipca 2025

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Artykuły w czasopismach na temat "Lunar Soft-Landing"

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Lin, Qing, and Jie Ren. "Investigation on the Horizontal Landing Velocity and Pitch Angle Impact on the Soft-Landing Dynamic Characteristics." International Journal of Aerospace Engineering 2022 (January 25, 2022): 1–16. http://dx.doi.org/10.1155/2022/3277581.

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The dynamic analysis of the soft landing of the lunar probe is very important to the design of the probe. The initial movement and attitude parameters of the probe during landing have a direct influence on the landing impact. In order to investigate the lunar probe soft-landing dynamic impact by different initial horizontal velocities, pitch angles, and inclinations of the lunar slope, an inertial force-based 7-DOF soft-landing dynamic model is applied under two conditions: the upward and downward slope landing surfaces. The impact on the dynamic characteristics of soft landing is analyzed in
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Kim, Yeong-Bae, Hyun-Jae Jeong, Shin-Mu Park, Jae Hyuk Lim, and Hoon-Hee Lee. "Prediction and Validation of Landing Stability of a Lunar Lander by a Classification Map Based on Touchdown Landing Dynamics’ Simulation Considering Soft Ground." Aerospace 8, no. 12 (2021): 380. http://dx.doi.org/10.3390/aerospace8120380.

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In this paper, a method for predicting the landing stability of a lunar lander by a classification map of the landing stability is proposed, considering the soft soil characteristics and the slope angle of the lunar surface. First, the landing stability condition in terms of the safe (=stable), sliding (=unstable), and tip-over (=statically unstable) possibilities was checked by dropping a lunar lander onto flat lunar surfaces through finite-element (FE) simulation according to the slope angle, friction coefficient, and soft/rigid ground, while the vertical touchdown velocity was maintained at
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Bojun, Zhang, and Liu Zhanchao. "Iterative Guidance Algorithm for Lunar Soft Landing." Journal of Physics: Conference Series 2235, no. 1 (2022): 012017. http://dx.doi.org/10.1088/1742-6596/2235/1/012017.

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Abstract A closed-form explicit guidance algorithm for the deceleration, attitude adjustment and final landing phases before lunar probe soft landing is presented in this paper. Guidance with a variable-thrust engine is extended from the iterative guidance mode (IGM) to satisfy the terminal velocity, position, and attitude constraints. The closed form expression, obtained by integrating the acceleration and shutdown time, is analysed to obtain an explicit ex-pression for the velocity and position requirements and vertical touchdown of the spacecraft toward a designated landing site with high t
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Banks, Michael. "Firefly Aerospace achieves lunar landing." Physics World 38, no. 4 (2025): 9iii. https://doi.org/10.1088/2058-7058/38/04/07.

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Shijie, Xu, and Zhu Jianfeng. "A new strategy for lunar soft landing." Journal of the Astronautical Sciences 55, no. 3 (2007): 373–87. http://dx.doi.org/10.1007/bf03256530.

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Qu, Mo Feng. "Lunar Soft - Landing Trajectory of Mechanics Optimization Based on the Improved Ant Colony Algorithm." Applied Mechanics and Materials 721 (December 2014): 446–49. http://dx.doi.org/10.4028/www.scientific.net/amm.721.446.

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Based on research carried out for the most fuel-lunar soft landing trajectory optimization problem. First, by improving the function approximation method, the lunar soft landing trajectory optimization problem into a parameter optimization problem, and the optimization variables and state variables have a clear physical meaning. Then use the decimal ant colony algorithm adds local search strategy to study the optimization problem. Finally, the optimization algorithm to optimize term direction angle simulation and error analysis.
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Wang, Dayi, Xiangyu Huang, and Yifeng Guan. "GNC system scheme for lunar soft landing spacecraft." Advances in Space Research 42, no. 2 (2008): 379–85. http://dx.doi.org/10.1016/j.asr.2007.08.031.

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Banerjee, Avijit, and Radhakant Padhi. "Multi-phase MPSP Guidance for Lunar Soft Landing." Transactions of the Indian National Academy of Engineering 5, no. 1 (2020): 61–74. http://dx.doi.org/10.1007/s41403-020-00090-1.

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Yin, Ke, Songlin Zhou, Qiao Sun, and Feng Gao. "Lunar Surface Fault-Tolerant Soft-Landing Performance and Experiment for a Six-Legged Movable Repetitive Lander." Sensors 21, no. 17 (2021): 5680. http://dx.doi.org/10.3390/s21175680.

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The cascading launch and cooperative work of lander and rover are the pivotal methods to achieve lunar zero-distance exploration. The separated design results in a heavy system mass that requires more launching costs and a limited exploration area that is restricted to the vicinity of the immovable lander. To solve this problem, we have designed a six-legged movable repetitive lander, called “HexaMRL”, which congenitally integrates the function of both the lander and rover. However, achieving a buffered landing after a failure of the integrated drive units (IDUs) in the harsh lunar environment
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Yuan, Qi, Heng Chen, Hong Nie, Guang Zheng, Chen Wang, and Likai Hao. "Soft-Landing Dynamic Analysis of a Manned Lunar Lander Em-Ploying Energy Absorption Materials of Carbon Nanotube Buckypaper." Materials 14, no. 20 (2021): 6202. http://dx.doi.org/10.3390/ma14206202.

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With the rapid development of the aerospace field, traditional energy absorption materials are becoming more and more inadequate and cannot meet the requirements of having a light weight, high energy absorption efficiency, and high energy absorption density. Since existing studies have shown that carbon nanotube (CNT) buckypaper is a promising candidate for energy absorption, owing to its extremely high energy absorption efficiency and remarkable mass density of energy absorption, this study explores the application of buckypaper as the landing buffer material in a manned lunar lander. Firstly
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Rozprawy doktorskie na temat "Lunar Soft-Landing"

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Hawkins, Alisa Michelle. "Constrained trajectory optimization of a soft lunar landing from a parking orbit." Thesis, Massachusetts Institute of Technology, 2005. http://hdl.handle.net/1721.1/32431.

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Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2005.<br>Includes bibliographical references (p. 141-144).<br>A trajectory optimization study for a soft landing on the Moon, which analyzed the effects of adding operationally based constraints on the behavior of the minimum fuel trajectory, has been completed. Metrics of trajectory evaluation included fuel expenditure, terminal attitude, thrust histories, etc.. The vehicle was initialized in a circular parking orbit and the trajectory divided into three distinct phases: de-orbit, descent, and braking
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Banerjee, Avijit. "Advanced Guidance and Autopilot Design for Autonomous Lunar Soft-Landing." Thesis, 2019. https://etd.iisc.ac.in/handle/2005/4397.

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Aiming towards the development of a long-term lunar research base for scientific exploration of futuristic objectives, soft-landing on the Moon has gained renewed interest worldwide. This work focuses on optimal guidance and autopilot design for multiphase autonomous soft-landing on the lunar surface. The objective of the guidance design is to translate the spacecraft from a parking-orbit towards the designated landing site with a near-zero touchdown velocity. In the process of the development, three different guidance methods that are capable of onboard implementation are explored. In this co
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Mathavaraj, S. "Innovative Optimal Guidance of Spacecrafts for Soft-Landing on Atmosphere-less Celestial Bodies." Thesis, 2019. https://etd.iisc.ac.in/handle/2005/4396.

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Nonlinear trajectory optimization based optimal guidance schemes are presented in this thesis for soft-landing of spacecrafts on atmosphere-less celestial bodies. First, a pseudo-spectral philosophy based multi-phase constrained fuel-optimal trajectory optimization problem for soft-landing on the closest celestial body (moon) is presented. The objective here is to find an optimal approach to successfully guide a spacecraft from the perilune of 18 km altitude of a transfer orbit to a height of 100 m over a specific landing site. The proposed approach takes into account various mission constrain
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Książki na temat "Lunar Soft-Landing"

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Zhang, He, Deng-Yun Yu, and Ze-Zhou Sun. Detector Technology of Lunar Soft Landing. Springer, 2020.

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Części książek na temat "Lunar Soft-Landing"

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Yu, Deng-Yun, Ze-Zhou Sun, and He Zhang. "Environment Analysis of Lunar Soft Landing Exploration." In Technology of Lunar Soft Lander. Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-15-6580-9_2.

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Pragallapati, Naveen, and N. V. S. L. Narasimham. "A TEP-Based Approach for Optimal Thrust Direction of Lunar Soft Landing." In Advances in Intelligent Systems and Computing. Springer Singapore, 2017. http://dx.doi.org/10.1007/978-981-10-3174-8_15.

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Yu, Deng-Yun, Ze-Zhou Sun, and He Zhang. "Landing Gear Technology of Lunar Lander." In Technology of Lunar Soft Lander. Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-15-6580-9_11.

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Streszczenia konferencji na temat "Lunar Soft-Landing"

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Zhiyuan Li and Hongjue Li. "Lunar soft landing trajectory optimization methods." In International Conference on Cyberspace Technology (CCT 2014). Institution of Engineering and Technology, 2014. http://dx.doi.org/10.1049/cp.2014.1365.

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Qiao, Yandi, Zexu Zhang, Feng Chen, Xingyan Wang, and Jing Wang. "Three-Dimensional Trajectory Optimization for soft lunar landing considering landing constraints*." In 2020 IEEE 16th International Conference on Control & Automation (ICCA). IEEE, 2020. http://dx.doi.org/10.1109/icca51439.2020.9264583.

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Jing-Yang, Zhou, Zhou Di, and Duan Guang-ren. "Optimal Orbit Design of Lunar Modules Soft Landing." In 2006 Chinese Control Conference. IEEE, 2006. http://dx.doi.org/10.1109/chicc.2006.280951.

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Songtao Chang, Yongji Wang, and Xing Wei. "Optimal soft lunar landing based on differential evolution." In 2013 IEEE International Conference on Industrial Technology (ICIT 2013). IEEE, 2013. http://dx.doi.org/10.1109/icit.2013.6505664.

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Zhou, Jingyang, Di Zhou, Kok Lay Teo, and Guohui Zhao. "Nonlinear optimal feedback control for lunar module soft landing." In 2009 IEEE International Conference on Automation and Logistics (ICAL). IEEE, 2009. http://dx.doi.org/10.1109/ical.2009.5262838.

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Huang, Xiangyu, and Dayi Wang. "Autonomous navigation and guidance for pinpoint lunar soft landing." In 2007 IEEE International Conference on Robotics and biomimetics (ROBIO). IEEE, 2007. http://dx.doi.org/10.1109/robio.2007.4522326.

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P, Amrutha V., Sreeja S, and Sabarinath A. "Trajectory Optimization of Lunar Soft Landing Using Differential Evolution." In 2021 IEEE Aerospace Conference. IEEE, 2021. http://dx.doi.org/10.1109/aero50100.2021.9438312.

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Banerjee, Avijit, and Radhakant Padhi. "Nonlinear Guidance and Autopilot Design for Lunar Soft Landing." In 2018 AIAA Guidance, Navigation, and Control Conference. American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-1872.

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Xu Xibao, Guo Jifeng, Bai Chengchao, and Zhang Luwen. "TV guidance technical schemes for manned lunar soft landing." In 2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC). IEEE, 2016. http://dx.doi.org/10.1109/cgncc.2016.7829158.

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Lin, Zhiyong. "The Control Strategy of Soft Landing Trajectory of Lunar Craft." In 2015 International conference on Applied Science and Engineering Innovation. Atlantis Press, 2015. http://dx.doi.org/10.2991/asei-15.2015.261.

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