Добірка наукової літератури з теми "Lunar Soft-Landing"
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Статті в журналах з теми "Lunar Soft-Landing"
Bojun, Zhang, and Liu Zhanchao. "Iterative Guidance Algorithm for Lunar Soft Landing." Journal of Physics: Conference Series 2235, no. 1 (May 1, 2022): 012017. http://dx.doi.org/10.1088/1742-6596/2235/1/012017.
Повний текст джерелаLin, 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.
Повний текст джерелаShijie, Xu, and Zhu Jianfeng. "A new strategy for lunar soft landing." Journal of the Astronautical Sciences 55, no. 3 (September 2007): 373–87. http://dx.doi.org/10.1007/bf03256530.
Повний текст джерелаKim, 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 (December 6, 2021): 380. http://dx.doi.org/10.3390/aerospace8120380.
Повний текст джерелаWang, Dayi, Xiangyu Huang, and Yifeng Guan. "GNC system scheme for lunar soft landing spacecraft." Advances in Space Research 42, no. 2 (July 2008): 379–85. http://dx.doi.org/10.1016/j.asr.2007.08.031.
Повний текст джерелаBanerjee, Avijit, and Radhakant Padhi. "Multi-phase MPSP Guidance for Lunar Soft Landing." Transactions of the Indian National Academy of Engineering 5, no. 1 (March 2020): 61–74. http://dx.doi.org/10.1007/s41403-020-00090-1.
Повний текст джерелаPark, Bong-Gyun, Jong-Sun Ahn, and Min-Jea Tahk. "Two-Dimensional Trajectory Optimization for Soft Lunar Landing Considering a Landing Site." International Journal of Aeronautical and Space Sciences 12, no. 3 (September 30, 2011): 288–95. http://dx.doi.org/10.5139/ijass.2011.12.3.288.
Повний текст джерелаQu, 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.
Повний текст джерелаYin, 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 (August 24, 2021): 5680. http://dx.doi.org/10.3390/s21175680.
Повний текст джерелаYuan, 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 (October 19, 2021): 6202. http://dx.doi.org/10.3390/ma14206202.
Повний текст джерелаДисертації з теми "Lunar Soft-Landing"
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.
Повний текст джерелаIncludes bibliographical references (p. 141-144).
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. Analysis was initially performed with two-dimensional translational motion, and the minimally constrained optimal trajectory was found to be operationally infeasible. Operational constraints, such as a positive descent orbit perilune height and a vertical terminal velocity, were imposed to obtain a viable trajectory, but the final vehicle attitude and landing approach angle remained largely horizontal. This motivated inclusion of attitude kinematics and constraints to the system. With rotational motion included, the optimal solution was feasible, but the trajectory still had undesirable characteristics. Constraining the throttle to maximum during braking produced a steeper approach, but used the most fuel. The results suggested a terminal vertical descent was a desirable fourth segment of the trajectory. which was imposed by first flying to an offset point and then enforcing a vertical descent, and provided extra safely margin prior to landing. In this research, the relative effects of adding operational constraints were documented and can be used as a baseline study for further detailed trajectory optimization.
by Alisa Michelle Hawkins.
S.M.
Книги з теми "Lunar Soft-Landing"
Zhang, He, Deng-Yun Yu, and Ze-Zhou Sun. Detector Technology of Lunar Soft Landing. Springer, 2020.
Знайти повний текст джерелаЧастини книг з теми "Lunar Soft-Landing"
Yu, Deng-Yun, Ze-Zhou Sun, and He Zhang. "Environment Analysis of Lunar Soft Landing Exploration." In Technology of Lunar Soft Lander, 21–49. Singapore: Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-15-6580-9_2.
Повний текст джерелаPragallapati, 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, 159–69. Singapore: Springer Singapore, 2017. http://dx.doi.org/10.1007/978-981-10-3174-8_15.
Повний текст джерелаYu, Deng-Yun, Ze-Zhou Sun, and He Zhang. "Landing Gear Technology of Lunar Lander." In Technology of Lunar Soft Lander, 367–99. Singapore: Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-15-6580-9_11.
Повний текст джерелаТези доповідей конференцій з теми "Lunar Soft-Landing"
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.
Повний текст джерелаQiao, 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.
Повний текст джерелаJing-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.
Повний текст джерелаSongtao 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.
Повний текст джерелаZhou, 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.
Повний текст джерелаHuang, 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.
Повний текст джерелаP, 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.
Повний текст джерелаBanerjee, Avijit, and Radhakant Padhi. "Nonlinear Guidance and Autopilot Design for Lunar Soft Landing." In 2018 AIAA Guidance, Navigation, and Control Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-1872.
Повний текст джерелаXu 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.
Повний текст джерелаLin, Zhiyong. "The Control Strategy of Soft Landing Trajectory of Lunar Craft." In 2015 International conference on Applied Science and Engineering Innovation. Paris, France: Atlantis Press, 2015. http://dx.doi.org/10.2991/asei-15.2015.261.
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