首页|基于自适应滑模控制的火箭炮运动控制器设计

基于自适应滑模控制的火箭炮运动控制器设计

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火箭炮系统因结构复杂、传动系统存在间隙、摩擦力难以准确计算,同时在炮弹发射过程中会产生系统质量和质心变化等问题,很难建立精确的火箭炮动力学模型来设计运动控制器.因此,基于模型的传统控制算法不易获得良好的控制效果.针对这一问题,提出了一种基于模糊控制的自适应滑模控制方法,与传统滑模控制方法对比分析,该方法在系统存在50 N·m固定值干扰和20%的不确定量共同作用的情况下,最大稳态误差为-2.38 × 10-3 rad.结果可知,模糊自适应滑模控制方法提高了控制系统的鲁棒性,使系统具有更高的自适应能力和抗干扰能力,仿真结果验证了该控制方法的可行性.
Design of rocket artillery motion controller based on adaptive sliding mode control
Currently,rocket artillery systems present challenges due to their complex structure,gaps in the transmission system,and the inherent difficulty in accurately calculating friction.Additionally,changes in system mass and center of gravity occur during projectile launch,complicating the establishment of a precise dynamic model for the design of motion controllers.Consequently,traditional control algorithms based on models encounter difficulties in achieving satisfactory control performance.To address these challenges,this paper proposes an adaptive sliding mode control method based on fuzzy control.Under conditions including a fixed disturbance of 50 N·m and a 20%uncertainty,this method exhibits a maximum steady-state error of-2.38 × 10-3 rad.The results indicate that the fuzzy adaptive sliding mode control enhances the robustness of the control system,allowing it to more effectively adapt to changes and resist disturbances.Simulation results further validate the feasibility of this innovative control approach.

rocket artillerysliding mode controlfuzzy controladaptive controltrajectory tracking

廖叶敏、尹海斌、肖郭城、张建新、张伟、刑秀敏

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武汉理工大学机电工程学院,武汉 430000

中国兵器工业集团江山重工研究院有限公司,湖北襄阳 441000

火箭炮 滑模控制 模糊控制 自适应控制 轨迹跟踪

国家自然科学基金重大研究计划项目"共融机器人"培育项目

91848102

2024

兵器装备工程学报
重庆市(四川省)兵工学会 重庆理工大学

兵器装备工程学报

CSTPCD北大核心
影响因子:0.478
ISSN:2096-2304
年,卷(期):2024.45(10)