A novel group decision-making （GDM） method based on intuitionistic fuzzy sets （IFSs） is developed to evaluate the ergonomics of aircraft cockpit display and control system （ACDCS）. The GDM process with four step...A novel group decision-making （GDM） method based on intuitionistic fuzzy sets （IFSs） is developed to evaluate the ergonomics of aircraft cockpit display and control system （ACDCS）. The GDM process with four steps is discussed. Firstly, approaches are proposed to transform four types of common judgement representations into a unified expression by the form of the IFS, and the features of unifications are analyzed. Then, the aggregation operator called the IFSs weighted averaging （IFSWA） operator is taken to synthesize decision-makers’ （DMs’） preferences by the form of the IFS. In this operator, the DM’s reliability weights factors are determined based on the distance measure between their preferences. Finally, an improved score function is used to rank alternatives and to get the best one. An illustrative example proves the proposed method is effective to valuate the ergonomics of the ACDCS.展开更多
目的探究稳定期精神分裂症患者的注意力特点。方法纳入55例稳定期精神分裂症患者和55名健康对照。采用注意网络测试范式(attention network test paradigm,ANT)对被试的注意力进行测评,观察指标包括4种提示线索和3种刺激类型下的反应时...目的探究稳定期精神分裂症患者的注意力特点。方法纳入55例稳定期精神分裂症患者和55名健康对照。采用注意网络测试范式(attention network test paradigm,ANT)对被试的注意力进行测评,观察指标包括4种提示线索和3种刺激类型下的反应时,以及换算后的3种注意网络(警觉网络、定向网络和执行控制网络)反应时。结果在不同提示线索和刺激类型下,患者组的反应时均高于对照组(P<0.001)。患者组的警觉网络反应时[25.43(11.71,42.53)ms vs.39.32(27.46,51.98)ms,P=0.020]和执行控制网络反应时[96.17(36.32,160.13)ms vs.44.43(18.52,89.73)ms,P<0.001]低于对照组,定向网络反应时在两组之间的差异无统计学意义(P=0.136)。结论稳定期精神分裂症患者的警觉网络和执行控制网络存在明显损伤,而定向网络未见明显损伤。展开更多
A new non-decoupling three-dimensional guidance law is proposed for bank-to-turn （BTT） missiles with the motion coupling problem. In this method, the different geometry is taken for theoretically modeling on B-IT mi...A new non-decoupling three-dimensional guidance law is proposed for bank-to-turn （BTT） missiles with the motion coupling problem. In this method, the different geometry is taken for theoretically modeling on B-IT missiles＇ motion within the threedimensional style without information loss, and meanwhile, Liegroup is utilized to describe the line-of-sight （LOS） azimuth when the terminal angular constraints are considered. Under these cir- cumstances, a guidance kinematics model is established based on differential geometry. Then, corresponding to no terminal angular constraint and terminal angular constraints, guidance laws are re- spectively designed by using proportional control and generalized proportional-derivative （PD） control in SO（3） group. Eventually, simulation results validate that this developed method can effectively avoid the complexity of pure Lie-group method and the information loss of the traditional decoupling method as well.展开更多
基金supported by the National Basic Research Program of China (973 Program) (2010CB734104)
文摘A novel group decision-making （GDM） method based on intuitionistic fuzzy sets （IFSs） is developed to evaluate the ergonomics of aircraft cockpit display and control system （ACDCS）. The GDM process with four steps is discussed. Firstly, approaches are proposed to transform four types of common judgement representations into a unified expression by the form of the IFS, and the features of unifications are analyzed. Then, the aggregation operator called the IFSs weighted averaging （IFSWA） operator is taken to synthesize decision-makers’ （DMs’） preferences by the form of the IFS. In this operator, the DM’s reliability weights factors are determined based on the distance measure between their preferences. Finally, an improved score function is used to rank alternatives and to get the best one. An illustrative example proves the proposed method is effective to valuate the ergonomics of the ACDCS.
基金supported by the National University of Defense Technology Innovation Support Project for Outstanding Graduate Student(B100303)
文摘A new non-decoupling three-dimensional guidance law is proposed for bank-to-turn （BTT） missiles with the motion coupling problem. In this method, the different geometry is taken for theoretically modeling on B-IT missiles＇ motion within the threedimensional style without information loss, and meanwhile, Liegroup is utilized to describe the line-of-sight （LOS） azimuth when the terminal angular constraints are considered. Under these cir- cumstances, a guidance kinematics model is established based on differential geometry. Then, corresponding to no terminal angular constraint and terminal angular constraints, guidance laws are re- spectively designed by using proportional control and generalized proportional-derivative （PD） control in SO（3） group. Eventually, simulation results validate that this developed method can effectively avoid the complexity of pure Lie-group method and the information loss of the traditional decoupling method as well.
文摘受到战争等特殊环境下部分节点导航拒止、节点移动性与环境干扰所带来的影响,快速进行测控网络拓扑重构是保证连续测控关键。为了解决上述问题,针对多体制无人集群测控网络的场景,提出一种基于多智能体深度确定性策略梯度(multi-agent deep deterministic policy gradient,MADDPG)的分布式多智能体测控网络群切换算法。该算法运用局部可观测马尔可夫决策模型,并考虑最小连通度、能耗与测控精度设计奖励函数,构建可靠的测控定位系统。仿真结果表明,该算法在不同的干扰环境下能有效抵抗外界干扰,保证测控定位的正常运行,与传统切换算法相比切换成功率提升12%以上。
