Статті в журналах з теми "Terminal guidance"
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Takehira, Tetsuya, Nguyen X. Vinh, and Pierre T. Kabamba. "Analytical Solution of Missile Terminal Guidance." Journal of Guidance, Control, and Dynamics 21, no. 2 (March 1998): 342–48. http://dx.doi.org/10.2514/2.4241.
Повний текст джерелаRusnak, Ilan. "Multiple Model-Based Terminal Guidance Law." Journal of Guidance, Control, and Dynamics 23, no. 4 (July 2000): 742–46. http://dx.doi.org/10.2514/2.4593.
Повний текст джерелаYu, Wenbin, Wanchun Chen, Liang Yang, Xiaoming Liu, and Hao Zhou. "Optimal terminal guidance for exoatmospheric interception." Chinese Journal of Aeronautics 29, no. 4 (August 2016): 1052–64. http://dx.doi.org/10.1016/j.cja.2016.04.019.
Повний текст джерелаLiaw, Der-Cherng, Yew-Wen Liang, and Chiz-Chung Cheng. "Nonlinear Control for Missile Terminal Guidance." Journal of Dynamic Systems, Measurement, and Control 122, no. 4 (February 4, 2000): 663–68. http://dx.doi.org/10.1115/1.1316796.
Повний текст джерелаCui, Yan Kai, Li Fu, Xiao Geng Liang, and Ling Luo. "Optimal Sliding-Mode Terminal Guidance Law Design of Airborne Boost-Phase Ballistic Missile Interception." Applied Mechanics and Materials 40-41 (November 2010): 15–20. http://dx.doi.org/10.4028/www.scientific.net/amm.40-41.15.
Повний текст джерелаGuo, Zhengyu, Chaolei Wang, Hang Qian, Zhiguo Han, and Jingxian Zhang. "Cooperative Intercepting Guidance Law for Large Maneuvering Target with Impact Angle Constraint." Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University 38, no. 6 (December 2020): 1257–65. http://dx.doi.org/10.1051/jnwpu/20203861257.
Повний текст джерелаUlybyshev, Yuri. "Terminal Guidance Law Based on Proportional Navigation." Journal of Guidance, Control, and Dynamics 28, no. 4 (July 2005): 821–24. http://dx.doi.org/10.2514/1.12545.
Повний текст джерелаHarl, Nathan, and S. N. Balakrishnan. "Reentry Terminal Guidance Through Sliding Mode Control." Journal of Guidance, Control, and Dynamics 33, no. 1 (January 2010): 186–99. http://dx.doi.org/10.2514/1.42654.
Повний текст джерелаAggarwal, Romesh K., and Charles R. Moore. "Terminal Guidance Algorithm for Ramjet-Powered Missiles." Journal of Guidance, Control, and Dynamics 21, no. 6 (November 1998): 862–66. http://dx.doi.org/10.2514/2.4349.
Повний текст джерелаKumar, Prem, Prasiddha N. Dwivedi, Abhijit Bhattacharyya, and Radhakant Padhi. "Terminal-Lead-Angle-Constrained Generalized Explicit Guidance." IEEE Transactions on Aerospace and Electronic Systems 53, no. 3 (June 2017): 1250–60. http://dx.doi.org/10.1109/taes.2017.2669598.
Повний текст джерелаZhou, Min, Jun Zhou, and Jianguo Guo. "Terminal area guidance for reusable launch vehicles." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 230, no. 2 (July 3, 2015): 333–49. http://dx.doi.org/10.1177/0954410015591615.
Повний текст джерелаLiang, Zixuan, Jiateng Long, Shengying Zhu, and Rui Xu. "Entry guidance with terminal approach angle constraint." Aerospace Science and Technology 102 (July 2020): 105876. http://dx.doi.org/10.1016/j.ast.2020.105876.
Повний текст джерелаMcInnes, Colin R. "Path shaping guidance for terminal lunar descent." Acta Astronautica 36, no. 7 (October 1995): 367–77. http://dx.doi.org/10.1016/0094-5765(95)00119-0.
Повний текст джерелаWang, Xingdan, Yu Yao, Baoqing Yang, and Jian Guo. "The Sensitivity Analysis of Difference Guidance Laws for the Terminal Guidance System." Advanced Science Letters 6, no. 1 (March 15, 2012): 346–50. http://dx.doi.org/10.1166/asl.2012.2323.
Повний текст джерелаCong, Mingyu, Xianghong Cheng, Zhiquan Zhao, and Zhijun Li. "Studies on Multi-Constraints Cooperative Guidance Method Based on Distributed MPC for Multi-Missiles." Applied Sciences 11, no. 22 (November 17, 2021): 10857. http://dx.doi.org/10.3390/app112210857.
Повний текст джерелаGao, C., J. Li, T. Feng, and W. Jing. "Adaptive terminal guidance law with impact-angle constraint." Aeronautical Journal 122, no. 1249 (November 29, 2017): 369–89. http://dx.doi.org/10.1017/aer.2017.124.
Повний текст джерелаShi, Qingli, Hua Wang, and Hao Cheng. "Multiple Constraints-Based Adaptive Three-Dimensional Back-Stepping Sliding Mode Guidance Law against a Maneuvering Target." Aerospace 9, no. 12 (December 5, 2022): 796. http://dx.doi.org/10.3390/aerospace9120796.
Повний текст джерелаZhe, Luo, Li Xinsan, Wang Lixin, and Shen Qiang. "Multiconstrained Gliding Guidance Based on Optimal and Reinforcement Learning Method." Mathematical Problems in Engineering 2021 (May 26, 2021): 1–12. http://dx.doi.org/10.1155/2021/6652232.
Повний текст джерелаYang, Fang, Kuanqiao Zhang, and Lei Yu. "Adaptive Super-Twisting Algorithm-Based Nonsingular Terminal Sliding Mode Guidance Law." Journal of Control Science and Engineering 2020 (July 4, 2020): 1–11. http://dx.doi.org/10.1155/2020/1058347.
Повний текст джерелаXu, X., and Y. Liang. "Biased optimal guidance law with specified velocity rendezvous angle constraint." Aeronautical Journal 119, no. 1220 (October 2015): 1287–99. http://dx.doi.org/10.1017/s0001924000011258.
Повний текст джерелаLiu, JH, JY Shan, and Q. Liu. "Optimal pulsed guidance law with terminal impact angle constraint." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 231, no. 11 (August 28, 2016): 1993–2005. http://dx.doi.org/10.1177/0954410016664918.
Повний текст джерелаXie, Dao Cheng, and Zhong Wei Wang. "Optimal Guidance Law Design for Reentry Vehicles with Terminal Velocity and Angle Constraints." Advanced Materials Research 459 (January 2012): 505–9. http://dx.doi.org/10.4028/www.scientific.net/amr.459.505.
Повний текст джерелаZhou, Hao, Tawfiqur Rahman, and Wanchun Chen. "Neural Network Assisted Inverse Dynamic Guidance for Terminally Constrained Entry Flight." Scientific World Journal 2014 (2014): 1–12. http://dx.doi.org/10.1155/2014/686040.
Повний текст джерелаPeng, Shuang Chun, Liang Pan, Tian Jiang Hu, and Lin Cheng Shen. "3D Nonlinear Guidance Law for Bank-to-Turn Missile." Advanced Materials Research 317-319 (August 2011): 727–33. http://dx.doi.org/10.4028/www.scientific.net/amr.317-319.727.
Повний текст джерелаWang, Hui, Jiang Wang, and Defu Lin. "Generalized optimal impact-angle-control guidance with terminal acceleration response constraint." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 231, no. 14 (September 11, 2017): 2515–36. http://dx.doi.org/10.1177/0954410017730250.
Повний текст джерелаQiao, Qing Qing, and Wan Chun Chen. "A Near Optimal Midcourse Guidance Law for Air-to-Air Missile." Applied Mechanics and Materials 336-338 (July 2013): 833–38. http://dx.doi.org/10.4028/www.scientific.net/amm.336-338.833.
Повний текст джерелаLi, E., and A. Fomichev. "Accuracy Analysis of Lunar Lander Terminal Guidance Algorithm." Science and Education of the Bauman MSTU 17, no. 04 (April 3, 2017): 113–28. http://dx.doi.org/10.7463/0417.0000957.
Повний текст джерелаRogers, Jonathan, and Nathan Slegers. "Robust Parafoil Terminal Guidance Using Massively Parallel Processing." Journal of Guidance, Control, and Dynamics 36, no. 5 (September 2013): 1336–45. http://dx.doi.org/10.2514/1.59782.
Повний текст джерелаRyoo, Chang-Kyung, Hangju Cho, and Min-Jea Tahk. "Optimal Guidance Laws with Terminal Impact Angle Constraint." Journal of Guidance, Control, and Dynamics 28, no. 4 (July 2005): 724–32. http://dx.doi.org/10.2514/1.8392.
Повний текст джерелаFowler, Lee, and Jonathan Rogers. "Bézier Curve Path Planning for Parafoil Terminal Guidance." Journal of Aerospace Information Systems 11, no. 5 (May 2014): 300–315. http://dx.doi.org/10.2514/1.i010124.
Повний текст джерелаFomichev, A. V., and E. K. Li. "Analytical 3D Terminal Guidance Algorithm for Lunar Landing." MEHATRONIKA, AVTOMATIZACIA, UPRAVLENIE 18, no. 6 (June 15, 2017): 423–31. http://dx.doi.org/10.17587/mau.18.423-431.
Повний текст джерелаLiang, Zixuan, Qingdong Li, and Zhang Ren. "Virtual Terminal–Based Adaptive Predictor–Corrector Entry Guidance." Journal of Aerospace Engineering 30, no. 4 (July 2017): 04017013. http://dx.doi.org/10.1061/(asce)as.1943-5525.0000716.
Повний текст джерелаXIANG, Shengwen, Tiancheng LI, Wei CHEN, Hongqi FAN, and Qiang FU. "Maximal admissible mode decision delay in terminal guidance." Chinese Journal of Aeronautics 32, no. 8 (August 2019): 1959–66. http://dx.doi.org/10.1016/j.cja.2019.02.011.
Повний текст джерелаFariz, A., and R. A. Sasongko. "Missile Initial Engagement Determination and Terminal Phase Guidance." IFAC-PapersOnLine 52, no. 12 (2019): 19–24. http://dx.doi.org/10.1016/j.ifacol.2019.11.063.
Повний текст джерелаVittal, R. Vijaya, and M. Seetharama Bhat. "Optimal explicit terminal guidance for a launch vehicle." Acta Astronautica 29, no. 4 (April 1993): 249–62. http://dx.doi.org/10.1016/0094-5765(93)90138-m.
Повний текст джерелаShieh, C. S. "Nonlinear rule-based controller for missile terminal guidance." IEE Proceedings - Control Theory and Applications 150, no. 1 (January 1, 2003): 45–48. http://dx.doi.org/10.1049/ip-cta:20030007.
Повний текст джерелаFan, Shijie, Hongqi Fan, Huaitie Xiao, Jianpeng Fan, and Qiang Fu. "Observability analysis of feature aided terminal guidance systems." Journal of Systems Engineering and Electronics 26, no. 1 (February 2015): 127–33. http://dx.doi.org/10.1109/jsee.2015.00017.
Повний текст джерелаLong, Jiateng, Ai Gao, Pingyuan Cui, and Yang Liu. "Mars atmospheric entry guidance for optimal terminal altitude." Acta Astronautica 155 (February 2019): 274–86. http://dx.doi.org/10.1016/j.actaastro.2018.12.001.
Повний текст джерелаRatnoo, Ashwini. "A Non-Switching Guidance Law with Terminal Constraints." IFAC-PapersOnLine 49, no. 1 (2016): 7–11. http://dx.doi.org/10.1016/j.ifacol.2016.03.020.
Повний текст джерелаJiang, C. W., G. F. Zhou, B. Yang, C. S. Gao, and W. X. Jing. "Novel guidance model and its application for optimal re-entry guidance." Aeronautical Journal 122, no. 1257 (October 2, 2018): 1811–25. http://dx.doi.org/10.1017/aer.2018.94.
Повний текст джерелаWu, Zhenglong, Zhenyu Guan, Chengwei Yang, and Jie Li. "Terminal Guidance Law for UAV Based on Receding Horizon Control Strategy." Complexity 2017 (2017): 1–19. http://dx.doi.org/10.1155/2017/2750172.
Повний текст джерелаZhang, Jing. "Research on Classroom Teaching Evaluation and Instruction System Based on GIS Mobile Terminal." Mobile Information Systems 2021 (July 15, 2021): 1–11. http://dx.doi.org/10.1155/2021/9790766.
Повний текст джерелаLi, Bin, Defu Lin, Jiang Wang, and Song Tian. "Guidance law to control impact angle and time based on optimality of error dynamics." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233, no. 10 (September 24, 2018): 3577–88. http://dx.doi.org/10.1177/0954410018801226.
Повний текст джерелаLi, Bin, Pan Tang, Haotian Xu, and Duo Zheng. "Terminal Impact Angle Control Guidance Law Considering Target Observability." Aerospace 9, no. 4 (April 3, 2022): 193. http://dx.doi.org/10.3390/aerospace9040193.
Повний текст джерелаGeng, Sheng-Tao, Jie Zhang, and Jing-Guang Sun. "Adaptive back-stepping sliding mode guidance laws with autopilot dynamics and acceleration saturation consideration." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233, no. 13 (March 19, 2019): 4853–63. http://dx.doi.org/10.1177/0954410019835728.
Повний текст джерелаKumar, G. N., and A. K. Sarkar. "CMAC Trained Optimum Mid course Guidance for Tactical Flight Vehicle." Defence Science Journal 71, no. 6 (October 22, 2021): 826–35. http://dx.doi.org/10.14429/dsj.71.16295.
Повний текст джерелаZhai, Qing Lin, Da Wei Lu, and Jun Zhang. "A Novel Decoupled LOS Rate Estimator for Terminal Guidance." Applied Mechanics and Materials 519-520 (February 2014): 1032–39. http://dx.doi.org/10.4028/www.scientific.net/amm.519-520.1032.
Повний текст джерелаKamalaskar, Mandar Bhanudas, S. Aditya Varma, and Mangal Kothari. "A nonlinear impact-angle guidance law." International Journal of Intelligent Unmanned Systems 5, no. 2/3 (April 19, 2017): 46–62. http://dx.doi.org/10.1108/ijius-03-2017-0003.
Повний текст джерелаZhang, Haoqiang, Shengjing Tang, and Jie Guo. "Cooperative near-space interceptor mid-course guidance law with terminal handover constraints." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233, no. 6 (May 3, 2018): 1960–76. http://dx.doi.org/10.1177/0954410018769182.
Повний текст джерелаde Celis, Raúl, Pablo Solano López, and Luis Cadarso. "Sensor hybridization using neural networks for rocket terminal guidance." Aerospace Science and Technology 111 (April 2021): 106527. http://dx.doi.org/10.1016/j.ast.2021.106527.
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