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基于高斯伪谱法的枪榴弹制导算法 被引量:1

Gaussian Pseudo-spectral Method for Smart Grenade Guidance
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摘要 针对目前枪榴弹制导算法稀少,传统中大口径弹药的制导方法不适用于枪榴弹制导等方面的问题,提出基于高斯伪谱法的枪榴弹制导算法。该算法利用高斯伪谱法规划出一条最优弹道作为标准弹道,依据实时弹道和标准弹道的偏差生成制导指令。以修正能量和制导精度为指标,对该算法进行仿真验证,结果表明该算法具有修正能量小、制导精度高的特点,易于在枪榴弹上实现与应用。 In response to the problems that the current grenade guidance algorithms are scarce and the traditional guidance methods for medium and large caliber ammunition were not applicable to grenade guidance,etc.,a grenade guidance algorithm based on Gaussian pseudo-spectral method was proposed.The algorithm used the Gaussian pseudo-spectral law to delineate an optimal trajectory as the standard trajectory,and generated guidance commands based on the deviation between the real-time trajectory and the standard trajectory.The algorithm simulation results were compared with those of the Gaussian pseudo-spectral-based guidance algorithm,the proportional guidance method and the drop-point prediction guidance method,and the results showed that the Gaussian pseudo-spectral based guidance algorithm in this paper had the characteristics of small correction energy and high guidance accuracy,and was easy to be implemented and applied to grenades.
作者 许一蒙 霍鹏飞 王超 雷泷杰 XU Yimeng;HUO Pengfei;LEI Longjie(Xi'an Institute of Electromechanical Information Technology,Xi'an 710065,China;Science and Technology on Electromechanical Dynamic Control Laboratory,Xi'an 710065,China)
出处 《探测与控制学报》 CSCD 北大核心 2023年第1期91-96,共6页 Journal of Detection & Control
关键词 枪榴弹 高斯伪谱法 弹道优化 制导与控制 grenade Gaussian pseudo-spectral method trajectory optimization guidance and control
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  • 1汪小娜,王树宗,朱华兵.火箭助推滑翔增程炮弹弹道模型研究[J].舰船科学技术,2005,27(1):77-79. 被引量:2
  • 2[1]Betts J T.Survey of numerical methods for trajectory optimization[J].Journal of Guidance,Control and Dynamics,1998,21(2):193-206.
  • 3[2]Ross I M,Fahroo F.A perspective on methods for trajectory optimization[C].In.AIAA/AAS Astrodynamics Specialist Conference and Exhibit.Monterey,CA,2002:1-7.
  • 4[3]Hull D G.Conversion of optimal control problems into parameter optimization problems[J].Journal of Guidance,Control and Dynamics,1997,20(1):57-60.
  • 5[4]Enright P J,Conway B A.Optimal finite-thrust spacecraft trajectories using collation and nonlinear programming[J].Journal of Guidance,Control and Dynamics,1991,10(5).
  • 6[10]Lu P.Inverse dynamics approach to trajectory optimization for an aerospace plane[J].Journal of Guidance,Control and Dynamics,1993,16(4):726-732.
  • 7[11]Bellman R E.Dynamic Programming[M].Princeton,USA:Princeton University Press,1957.
  • 8[13]Luus R.Iterative dynamic programming:from curiosity to a practical optimization procedure[J].Control and Intelligent Systems,1998,26:1-8.
  • 9[14]Bousson K.Single Gridpoint Dynamic Programming for trajectory Optimization[C].In.AIAA Atmospheric Flight Mechanics Conference and Exhibit.San Francisco,California,2005:1-8.
  • 10[15]Adam W,Tim C,Ellen B.Genetic algorithm and calculus of variations-based trajectory optimization technique[J].Journal of Spacecraft and Rockets,2003,40(6):882-888.

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