Optimization of lunar soft landing trajectory based on hybrid method
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摘要: 利用混合法思想和人工免疫算法研究了月球软着陆轨迹优化问题.首先建立月球软着陆系统模型并进行归一化处理;然后基于混合法思想利用庞特亚金(Pontryagin)极大值原理推导最优控制律,以伴随变量初值和终端时刻作为优化变量,将终端约束作为罚函数引入评价函数中,将月球软着陆轨迹优化问题转化为非线性规划问题(NLP,Nonlinear Programming);最后应用引导人工免疫算法(GAIA,Guiding Artificial Immune Algorithm)求解该优化问题.仿真结果表明,GAIA混合算法比直接法的寻优速度快,终端误差小,且可搜索到理论最优轨迹;同时,GAIA混合算法的伴随变量初值收敛范围比间接法大,降低了最优月球软着陆轨迹的搜索难度.Abstract: The lunar soft landing trajectory was optimized by hybrid method and artificial immune algorithm (AIA). Firstly, the system model of lunar soft landing trajectory was established and normalized. Secondly, the optimization problem of lunar soft landing trajectory was converted into a nonlinear programming (NLP) via hybrid method, in which optimal control law was derived by Pontryagin's maximum principle, the initial values of adjoint variables and terminal time were variables to be optimized, and terminal constraints were introduced into evaluation function as penalty terms. Finally, a guiding artificial immune algorithm (GAIA) was applied to solve this optimization problem. Simulation results show that the GAIA hybrid method has faster optimization speed and higher optimization precision than direct method, and can obtain the theoretical optimal trajectory. Meanwhile, GAIA hybrid method has larger convergence range of initial value of adjoint variables than indirect method, and reduces the difficulty of searching optimal lunar soft landing trajectory.
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[1] Lee A Y. Fuel-efficient descent and landing guidance logic for a safe lunar touchdown[C]//AIAA Guidance, Navigation, and Control Conference.Reston, VA:American Institute of Aeronautics and Astronautics Inc, 2011:4978-4999 [2] Biegler L T. An overview of simultaneous strategies for dynamic optimization[J].Chemical Engineering and Processing:Process Intensification, 2007, 46(11):1043-1053 [3] 王大轶, 李铁寿, 马兴瑞.月球最优软着陆两点边值问题的数值解法[J].航天控制, 2000(3):44-49 Wang Dayi, Li Tieshou, Ma Xingrui.Numerical solution of TPBVP in optimal lunar soft landing[J].Aerospace Control, 2000(3): 44-49(in Chinese) [4] 赵吉松, 谷良贤, 潘雷.月球最优软着陆两点边值问题的数值解法[J].中国空间科学技术, 2009, 29(4):21-27 Zhao Jisong, Gu Liangxian, Pan Lei.Numerical solution of TPBVP for optimal lunar soft landing[J].Chinese Space Science and Technology, 2009, 29(4):21-27(in Chinese) [5] 王劼, 崔乃刚, 刘暾, 等.定常推力登月飞行器最优软着陆轨道研究[J].高技术通讯, 2003, 13(4):39-42 Wang Jie, Cui Naigang, Liu Tun, et al.Study on soft-landing trajectories of constant-thrust-amplitude lunar probe[J].High Technology Letters, 2003, 13(4):39-42(in Chinese) [6] 王劼, 李俊峰, 崔乃刚, 等.登月飞行器软着陆轨道的遗传算法优化[J].清华大学学报:自然科学版, 2003, 43(8):1056-1059 Wang Jie, Li Junfeng, Cui Naigang, et al.Genetic algorithm optimization of lunar probe soft-landing trajectories[J].Journal of Tsinghua University:Science and Technology, 2003, 43(8):1056-1059(in Chinese) [7] 朱建丰, 徐世杰. 基于自适应模拟退火遗传算法的月球软着陆轨道优化[J].航空学报, 2007, 28(4):806-812 Zhu Jianfeng, Xu Shijie.Optimization of lunar soft landing trajectory based on adaptive simulated annealing genetic algorithm[J].Acta Aeronautica et Astronautica Sinica, 2007, 28(4):806-812(in Chinese) [8] 段佳佳, 徐世杰, 朱建丰.基于蚁群算法的月球软着陆轨迹优化[J].宇航学报, 2008, 29(2):476-481 Duan Jiajia, Xu Shijie, Zhu Jianfeng.Optimization of lunar soft landing trajectory based on ant colony algorithm[J].Journal of Astronautics, 2008, 29(2):476-481(in Chinese) [9] 孙军伟, 乔栋, 崔平远.基于SQP方法的常推力月球软着陆轨道优化方法[J].宇航学报, 2006, 27(1):99-102 Sun Junwei, Qiao Dong, Cui Pingyuan.Study on the optimal trajectories of lunar soft-landing with fixed-thrust using SQP method[J].Journal of Astronautics, 2006, 27(1):99-102(in Chinese) [10] 彭祺擘, 李海阳, 沈红新.基于高斯-伪谱法的月球定点着陆轨道快速优化设计[J].宇航学报, 2010, 31(4):1012-1016 Peng Qibo, Li Haiyang, Shen Hongxin.Rapid lunar exact-landing trajectory optimization via gauss pseudospectral method[J].Journal of Astronautics, 2010, 31(4):1012-1016(in Chinese) [11] 单永正, 段广仁, 张烽.月球精确定点软着陆轨道设计及初始点选取[J].宇航学报, 2009, 30(6):2099-2104 Shan Yongzheng, Duan Guangren, Zhang Feng.Orbit design of lunar precise fixed-point soft landing and selection of initial point[J].Journal of Astronautics, 2009, 30(6):2099-2104(in Chinese) [12] 梁栋, 刘良栋, 何英姿.月球精确软着陆李雅普诺夫稳定制导律[J].中国空间科学技术, 2011, 31(2):25-31 Liang Dong, Liu Liangdong, He Yingzi.Guidance law for lunar pinpoint soft landing based on lyapunov stability theory[J].Chinese Space Science and Technology, 2011, 31(2):25-31(in Chinese) [13] 王明光, 裴听国, 袁建平.基于伪光谱方法月球软着陆轨道快速优化设计[J].中国空间科学技术, 2007, 27(5):27-32 Wang Mingguang, Pei Tingguo, Yuan Jianping.Legendre pseudospectral method for rapid lunar soft-landing trajectory optimization[J].Chinese Space Science and Technology, 2007, 27(5): 27-32(in Chinese) [14] 赵吉松, 谷良贤. 基于广义乘子法的月球软着陆轨道快速优化设计[J].科技导报, 2008, 26(20):50-54 Zhao Jisong, Gu Liangxian.Rapid optimization of lunar soft landing trajectory based on generalized lagrange multiplier[J].Science & Technology Review, 2008, 26(20):50-54(in Chinese) [15] 单永正, 段广仁. 应用非线性规划求解月球探测器软着陆最优控制问题[C]//第二十六届中国控制会议论文集.北京:北京航空航天大学出版社, 2007:485-487 Shan Yongzheng, Duan Guangren.Applying nonlinear programming to solve optimal control problem of lunar probe soft landing[C]//Proceeding of the 26th Chinese Control Conference, Beijing:Beihang University Press, 2007:485-487(in Chinese) [16] 曹涛, 董长虹. 基于组合优化策略的月球软着陆最优轨道设计[J].北京航空航天大学学报, 2012, 38(11):1537-1541 Cao Tao, Dong Changhong.Optimization of lunar soft landing trajectory based on combinational algorithm[J].Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(11):1537-1541(in Chinese) [17] 彭坤, 徐世杰, 果琳丽, 等.基于人工免疫算法的地球-火星小推力转移轨道优化[J].中国空间科学技术, 2012, 32(5): 61-68 Peng Kun, Xu Shijie, Guo Linli, et al.Optimization of Earth-Mars low-thrust trajectory based on artificial immune algorithm[J].Chinese Space Science and Technology, 2012, 32(5):61-68(in Chinese)
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