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Functional transformations of images in neural networks 神经网络中图像的函数变换
Pub Date : 1900-01-01 DOI: 10.18127/j20700814-202205-04
V. V. Kvashennikov
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引用次数: 0
Determination of the permissible level of degradation of the multiprocessor matrix of the information and control system 信息和控制系统的多处理机矩阵的允许退化水平的测定
Pub Date : 1900-01-01 DOI: 10.18127/20700814-202201-10
A. Ulasen, O. Andreeva, S.Kh. Ekshembiev, E. G. Berger
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引用次数: 0
Algorithm for maintaining the energy balance of the power supply system of the earth remote sensing spacecraft under critical operating conditions 关键工况下地球遥感航天器供电系统能量平衡维持算法
Pub Date : 1900-01-01 DOI: 10.18127/j20700814-202103-02
G. B. Steganov, Yury Chudnovsky, N. Alimov, A.A. Skoptsov
In this paper, we consider the problem of maintaining the energy balance of the power supply system of the Earth remote sensing spacecraft in critical operating conditions with the most intense cyclogram of the spacecraft operation, the maximum state of degradation of energy sources and storage devices, as well as with the minimum time to replenish useful energy.The problem of maintaining balance is formulated as a problem of nonlinear mathematical programming with functional constraints. Goal of the work is improving the efficiency and survivability of the remote sensing spacecraft and maintaining the energy balance of the power system in critical operating conditions by transferring the storage devices of the accumulating subsystem of the spacecraft to a given level of charge in the minimum charge time. An algorithm for controlling the accelerated charge of the rechargeable battery with the analysis of the Nickel-hydrogen battery temperature and its time derivative is developed.in some cases, the rechargeable battery replenishment time was reduced by 12−20%. The proposed algorithm for maintaining the energy balance can be used to select the stages of the accumulating subsystem charge current and transition from the current stage to the next one in a minimum time, providing flexibility in managing the modes of electricity storage with the adaptation of the charging current profiles to changing critical operating conditions.
本文考虑了在航天器运行周期最剧烈、能量源和存储设备退化状态最大、可用能量补充时间最短的关键工况下,地球遥感航天器供电系统能量平衡的维持问题。将平衡问题表述为具有函数约束的非线性数学规划问题。该工作的目的是通过在最短的充电时间内将航天器积累分系统的存储装置转移到给定的充电水平,提高遥感航天器的工作效率和生存能力,并在关键运行条件下保持动力系统的能量平衡。通过对镍氢电池温度及其时间导数的分析,提出了一种控制可充电电池加速充电的算法。在某些情况下,可充电电池的补充时间减少了12 - 20%。所提出的能量平衡维持算法可用于选择累积子系统充电电流的阶段,并在最短时间内从当前阶段过渡到下一阶段,通过调整充电电流分布以适应关键运行条件的变化,为管理蓄电模式提供了灵活性。
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引用次数: 0
Mathematical model of the thermal imaging seeker of an air-to-air guided missile 空空导弹热成像导引头的数学模型
Pub Date : 1900-01-01 DOI: 10.18127/j20700814-202204-07
S.M. Lazarenkov, E. D. Shatsky
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引用次数: 0
Mathematical modeling of thermophysical processes in thermocathodes of high-current plasma systems 大电流等离子体系统热阴极热物理过程的数学建模
Pub Date : 1900-01-01 DOI: 10.18127/j20700814-202206-05
I.K. Belova, E.O. Deryuginа, I.V. Сhukhraev
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引用次数: 0
Algorithmic support of low-altitude aircraft flight based on the hazard analysis of the flight situation 基于飞行态势危害分析的低空飞机飞行算法支持
Pub Date : 1900-01-01 DOI: 10.18127/j20700814-202104-03
V. Malyshev, A. S. Leontyev, S. P. Poluektov, Е.М. Volotov
Low-altitude flight of an aircraft is an effective, but at the same time, a very complex tactical technique, during which the crew does not always have the opportunity to timely recognize the occurrence of an abnormal case, determine the way out of it and counteract an aviation accident development. Despite many advantages of the automatic mode of low-altitude flight performing, its practical implementation is associated with a number of features and disadvantages, which determined the preference for the manual mode of low-altitude flight control. These are the presence of telltale factors, limited ability of performing flights at night and in difficult weather conditions, insufficient reliability etc. The considered features determined the relevance of the of low-altitude flight safety ensuring problem in relation to the manual control mode. As a result of an experimental study of the low-altitude flight performing process in a manual control mode, it was found that when performing manually-controlled low-altitude flight, a hazard assessment of the flight situation becomes pivotal. However the crew being under such conditions is not always able to correctly assess the flight situation hazard due to a combination of objective reasons. The current state of the adaptive and on-board flight safety systems theory makes it possible to increase the safety of the manuallycontrolled low-altitude flight by using adaptive control algorithms based on the flight situation hazard assessment. To solve this problem an adaptive control algorithm is proposed that ensures the formation of a security corridor in the longitudinal control channel, where the upper limit is determined by the critical value of the aircraft detection hazard, and the lower limit is determined by the critical value of the error in maintaining a given flight altitude. For a continuous assessment of the flight situation hazard and the timely formation of control signals the complex information about the current true flight altitude and the foreground is needed. Taking into account the peculiarities of low-altitude flight a digital terrain map containing data on natural and artificial obstacles along the flight route is a more rational source of information, that will make it possible to predict the development of the flight situation hazard. The above reasoning makes it possible to form an aircraft low-altitude flight adaptive control algorithm. A distinctive feature of the proposed algorithm is the implementation of a combined control variety where the pilot is provided with ample manual control opportunities within the security corridor, and the automatic flight control system is assigned the role of a safety subsystem that ensures control and timely return of the flight situation to normal flight conditions. The presented algorithm will allow to increase the crew logical-analytical activity information support during continuous analysis of the existing flight situation due to the formatio
飞机的低空飞行是一种有效的,但同时也是一种非常复杂的战术技术,在此过程中,机组人员并不总是有机会及时识别异常情况的发生,确定摆脱异常情况的方法,并应对航空事故的发展。尽管低空飞行执行自动模式具有许多优点,但其实际实施中存在许多特点和缺点,这决定了人们对低空飞行控制手动模式的偏好。这些因素包括:存在一些暴露的因素,在夜间和恶劣天气条件下执行飞行的能力有限,可靠性不足等。所考虑的特点决定了低空飞行安全保障问题与手动控制方式的相关性。通过对手控模式下低空飞行执行过程的实验研究,发现在进行手控低空飞行时,对飞行态势进行危险评估是关键。然而,由于客观原因的综合作用,机组人员在这种情况下并不总是能够正确地评估飞行状况危险。自适应和机载飞行安全系统理论的现状使得基于飞行态势危害评估的自适应控制算法能够提高人工控制低空飞行的安全性。针对这一问题,提出了一种保证纵向控制通道形成安全通道的自适应控制算法,其上限由飞机探测危险的临界值确定,下限由保持给定飞行高度误差的临界值确定。为了对飞行态势危害进行持续评估,及时形成控制信号,需要有关当前真实飞行高度和前景的复杂信息。考虑到低空飞行的特点,包含飞行路线沿线自然和人工障碍物数据的数字地形图是一种更合理的信息来源,可以预测飞行态势危险的发展。上述推理使飞机低空飞行自适应控制算法的形成成为可能。该算法的一个显著特点是实现了一种组合控制方式,在安全通道内为飞行员提供了充足的手动控制机会,自动飞行控制系统被赋予安全子系统的角色,以确保控制并及时将飞行状况恢复到正常飞行状态。所提出的算法将允许在现有飞行情况的持续分析中增加机组逻辑分析活动信息支持,因为基于当前飞行情况危害分析形成保护性控制行动。
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引用次数: 0
Synthesis and research of filter with a variation of coefficients for tracking a maneuvering aerodynamic target 机动气动目标跟踪变系数滤波器的合成与研究
Pub Date : 1900-01-01 DOI: 10.18127/j20700814-202106-02
U.A. Apоrovich
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引用次数: 0
Fundamentals of building the intellectual architecture training systems for specialists on the application of radio electronic objects 无线电电子对象应用专家智力架构训练系统之建立基础
Pub Date : 1900-01-01 DOI: 10.18127/j20700814-202201-06
L. Mistrov, O. V. Polyakov, V.M. Shatskikh
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引用次数: 0
Set-theoretical model of homeostasis of group activity of operators of ergatic systems in conditions of negative impact environmental factors 负面环境因素影响下电系统操作者群体活动稳态的集合理论模型
Pub Date : 1900-01-01 DOI: 10.18127/j20700814-202102-04
S. Bagretsov, A. Danilov, V. Aldokhina, S.A. Zyrin, I.O. Sharapov
Among the most significant system properties of such complex technical objects as man-machine complexes, it should be noted the possibility of unauthorized actions of operators or control personnel in subjectively difficult situations. During operation, these properties determine the need to consider the area of potential situations of control of man-machine complexes that were not provided for by the developers during the design.Traditionally, this problem arises at the stage of the operation of the complexes, when situations of the system functioning unforeseen by the developers arise from time to time. Further, they form the basis of projects for the modernization or improvement of this type of equipment. The purpose of this work is to consider the constructive conceptual apparatus, methods of analysis, including formal means of identifying and assessing the functional redundancy of organizational structures of operational management systems and to develop principles for its use to ensure the homeostaticity of group activities of operators in conditions of negative influence of environmental factors. The article systematizes the basic concepts and definitions of homeostasis of group activity of operators of control groups of modern man-machine complexes. On the basis of the set-theoretic model, the conditions for increasing the stability of the activity of a group of operators in conditions of the negative impact of external factors are determined. The set-theoretical analysis of the functionally redundant organizational structure of operational management systems carried out in the article makes it possible to determine the conditions and mechanisms for expanding the area of homeostasis of the functioning of the organizational structures of control systems, the implementation of which is associated with the methods of coordinating and motivational influence on operators, improving the structure of their information and functional interactions and substitutions (emulation) of the functions of the operators of the degrading control group.
在人机综合体等复杂技术对象的最重要的系统特性中,应该注意操作员或控制人员在主观困难情况下未经授权操作的可能性。在操作过程中,这些属性决定了需要考虑开发人员在设计过程中没有提供的人机综合体控制的潜在情况。传统上,这个问题出现在综合体的操作阶段,当开发人员无法预见的系统功能情况不时出现时。此外,它们构成了这类设备现代化或改进项目的基础。这项工作的目的是考虑建设性的概念装置,分析方法,包括识别和评估运营管理系统组织结构的功能冗余的正式方法,并制定其使用原则,以确保操作员在环境因素负面影响条件下的群体活动的稳态。本文系统地介绍了现代人机综合体控制组操作者群体活动动态平衡的基本概念和定义。在集合论模型的基础上,确定了在外部因素产生负面影响的情况下,增加一群算子活动稳定性的条件。本文对运营管理系统的功能冗余组织结构进行了集合理论分析,从而可以确定扩大控制系统组织结构功能的稳态区域的条件和机制,其实施与对操作员的协调和激励影响方法有关。改进它们的信息结构和功能相互作用,替换(仿真)退化控制组的操作员的功能。
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引用次数: 0
Frequency characteristics surfaces of control systems complexvalued transfer functions 控制系统复值传递函数的频率特性曲面
Pub Date : 1900-01-01 DOI: 10.18127/j20700814-202105-05
Yu. P. Kornyushin, E. Klimanova, A. V. Maksimov
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引用次数: 0
期刊
Information-measuring and Control Systems
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