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战斗机人工势场在主从编队引导控制中的应用 被引量:5
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作者 魏贤智 庞春雨 +1 位作者 孙亮 周焘 《电光与控制》 北大核心 2010年第3期51-56,共6页
引入战斗机人工势场的概念,建立针对主从编队引导控制的模型。在分析势、势场力的基础上,构建战斗机编队的队形势以及队形力函数。建立编队控制模型,编队队形的结构与队形参考点有关,参考点的数量和位置由队形和队形控制方式决定,主从... 引入战斗机人工势场的概念,建立针对主从编队引导控制的模型。在分析势、势场力的基础上,构建战斗机编队的队形势以及队形力函数。建立编队控制模型,编队队形的结构与队形参考点有关,参考点的数量和位置由队形和队形控制方式决定,主从编队控制以长机为队形参考点。建立了基于队形力的主从编队控制模型,并应用于实际领航者之中。仿真表明飞行误差收敛速度快,僚机能够稳定跟踪领航者的飞行轨迹,并保持较小的跟踪误差(20~40m)。在密集编队控制中,仍需改进控制器和优化参数;在稀疏队形和分散队形中,完全可以满足控制需要。 展开更多
关键词 战斗机人工势场 编队控制 主从编队控制 队形 队形力 参考点
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Formation keeping control through inter-satellite electromagnetic force 被引量:4
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作者 CAI WeiWei YANG LePing +1 位作者 ZHU YanWei ZHANG YuanWen 《Science China(Technological Sciences)》 SCIE EI CAS 2013年第5期1102-1111,共10页
Satellite formation keeping through inter-satellite electromagnetic force provides an attractive alternative for future space missions due to its distinct advantages of no propellant consumption or plume contamination... Satellite formation keeping through inter-satellite electromagnetic force provides an attractive alternative for future space missions due to its distinct advantages of no propellant consumption or plume contamination as compared to conventional approaches.However,the internal force nature as well as the high nonlinearity and coupling of electromagnetic force brings new control challenges for this novel technique.In this paper,analysis on the dynamics characteristics and special control issues in the presence of electromagnetic force is carried out on the basis of the derived relatively translational dynamics.Considering the model uncertainties,external disturbances and sensor noise,a combined nonlinear control scheme involving feed-forward and feedback control components is proposed for electromagnetic-force-based formation keeping.The feed-forward component is directly obtained through desired configuration and dynamics under nominal conditions while the feedback component is realized utilizing active disturbance rejection control methodology with some reasonable improvement.Numerical simulation is presented to verify the feasibility and validity of the combined control scheme. 展开更多
关键词 inter-satellite electromagnetic force formation keeping dynamics analysis active disturbance rejection nonlinear control
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