航空动力装置任务可靠度模糊预计与分配的综合

根据Vague集的直觉性，定义一种判定Vague值真值的函数，进而给出一种确定Fuzzy隶属度的方法。将此方法应用于模糊综合评判理论，得到一种在设计初期根据专家意见，预计航空动力装置任务可靠度的模糊决策方法。根据预计值和比例组合分配法的思想，先按任务可靠度模型的等效串联模型进行任务可靠度指标的分配，然后再对等效串联模型中冗余部分的指标进行分配。     

基于改进DQN的复合模式在轨服务资源分配

针对开展在轨服务前的资源分配非线性多目标优化问题，构建复合服务模式下的在轨资源分配模型，基于对DQN （Deep Q-Network）方法的收敛性和稳定性改进，提出了一种在轨服务资源分配方法。该方法能够应对同时包含"一对多""多对一"的复合服务模式，并在满足预期成功率的前提下优先分配重要服务对象，兼顾资源分配综合效益和总体能耗效率，达到了以期望成功率、较少资源投入尽快完成任务的综合目标。仿真实验表明，改进DQN方法能够在任务执行前依据服务对象重要程度自主分配航天器资源，收敛速度快、训练误差低，在分配效益和总体能耗的优化方面具有明显的比较优势。     

“六性”、“七化”与“一品”——全国高职高专学报走向再探索

通过分析高职高专学报生存发展的现状和面临的主要问题,提出了高职高专学报的宗旨定位、作者定位、读者定位和特色定位;结合学报学会组织的功能和使命及高职高专学报的发展方向,归结出了“六性”、“七化”与“一品”的奋斗目标。     

VLIW上的软件旁路与细粒度并行调度

描述并分析了一种新型的VLIW(Very Long Instruction Word)机器模型,为充分利用该模型的并行特性,提出了基于静态单一赋值(SSA)表示的软件旁路方法,以及集成的基于操作的指令调度与寄存器分配算法.与常规的软件旁路方法和基于周期的调度方法相比,该方法可以灵活地进行结果寄存器的分配,并有效减少由重用结果寄存器导致的"危险值"溢出次数,生成高质量的目标代码.      

基于飞行性能最优的多操纵面飞机配平研究

从飞行性能最优的角度,对多操纵面飞机的配平原则与算法进行了研究。以瑞典FO I开发的ADM IRE为例,根据所建立的配平原则与算法对其进行了重新配平。比较了新配平方法与原配平方法的飞行性能,结果证实采用新配平方法的飞机飞行性能较好,说明所建立的配平原则与方法是合理的。     

An allowance allocation method based on dynamic approximation via online inspection data for deformation control of structural parts

Deformation resulting from residual stress has been a significant issue in machining. As allowance allocation can directly impact the residual stress on part deformation, it is essential for deformation control. However, it is difficult to adjust allowance allocation by traditional simulation methods based on residual stress, as the residual stress cannot be accurately measured or predicted, and many unexpected factors during machining process cannot be simulated accurately. Different from traditional methods, this paper proposes an allowance allocation method based on dynamic approximation via online inspection data for deformation control of structural parts. An Autoregressive Integrated Moving Average (ARIMA) model for dynamic allowance allocation is established so as to approach the minimum deformation, which is based on the in-process deformation inspection data during the alternative machining process of upside and downside. The effectiveness of the method is verified both by simulation cases and real machining experiments of aircraft structural parts, and the results show that part deformation can be significantly reduced.     

帕累托最优与航空客运中的超售

通过对超售产生和发展过程中不断的效率改进的分析，说明超售实际上具有不断优化配置资源的作用，不断逼近理论参照体系中的帕累托最优，从而使航空公司和旅客双方受益。同时，探讨了我国航空公司应如何开展超售，以提高航空公司资源使用的效率。     

飞翼布局无人机的稳定与操纵特性分析研究

从气动和控制综合设计角度,提出了解决飞翼布局无人机稳定能力问题的多轴静不稳定增稳控制规律,通过对多操纵面操纵特性和操纵需求分析给出了操纵面的配置策略.仿真分析表明,所提出的设计方法较好地解决了飞翼布局无人机特殊的稳定与操纵问题.     

Finite-time sliding mode attitude control for a reentry vehicle with blended aerodynamic surfaces and a reaction control system

This paper proposes a finite-time robust flight controller, targeting for a reentry vehicle with blended aerodynamic surfaces and a reaction control system(RCS). Firstly, a novel finite-time attitude controller is pointed out with the introduction of a nonsingular finite-time sliding mode manifold. The attitude tracking errors are mathematically proved to converge to zero within finite time which can be estimated. In order to improve the performance, a second-order finite-time sliding mode controller is further developed to effectively alleviate chattering without any deterioration of robustness and accuracy. Moreover, an optimization control allocation algorithm, using linear programming and a pulse-width pulse-frequency(PWPF) modulator, is designed to allocate torque commands for all the aerodynamic surface deflections and on–off switching-states of RCS thrusters.Simulations are provided for the reentry vehicle considering uncertain parameters and external disturbances for practical purposes, and the results demonstrate the effectiveness and robustness of the attitude control system.     

基于MILP的多无人机对敌防空火力压制

建立了基于混合整数线性规划（Mixed Integer LinearProgram,MILP）的多无人机编队对敌防空火力压制协同任务分配模型,以0-1决策变量表征无人机一任务指派关系,引入连续时间决策变量来表示任务的执行时间,并通过对决策变量之间的线性等式和不等式的数学描述,建立无人机之间和无人机执行任务之间合理的协同约束关系。采用商用软件CPLEX对模型求解,仿真验证了模型的合理性。