多Agent航天自主运行系统的模型描述

来源 :航天控制 | 被引量 : 0次 | 上传用户:dx0746
下载到本地 , 更方便阅读
声明 : 本文档内容版权归属内容提供方 , 如果您对本文有版权争议 , 可与客服联系进行内容授权或下架
论文部分内容阅读
针对基于多Agent的航天自主运行系统,梳理了模型描述的内容和要求。为了满足多Agent之间协同规划以及Agent内部自主规划的要求,提出了活动和方案两级的规划系统描述模型。在活动一级建立与时间、资源的约束关系,实现Agent之间的规划分解、交互协商。以方案描述系统组成部分的运行状态,并通过方案衔接约束和能量参数的定义,使Agent具有局部优化和适应变化的能力。使用选择性约束和优先级等参数,使规划活动更为灵活和鲁棒。Agent知识描述语言使用类似C++的语法,使用预定义类和函数来实现规划知识的描述,方便实现过程性运算,易于扩展。通过规划模型描述的实例验证了描述语言的描述能力。模型语言的处理程序已经应用于仿真系统,可以针对应用场景进行仿真。 Aiming at the autonomous system of aerospace based on multi-agent, the contents and requirements of model description are summarized. In order to meet the requirements of coordinated planning among multi-agents and autonomous planning within the agents, a planning system description model of activities and schemes is proposed. At the activity level, it establishes the constraint relation with time and resources to realize the planning decomposition and mutual negotiation between Agents. The program states the operating status of the system components, and through the definition of the protocol convergence constraints and energy parameters, the Agent has the ability of local optimization and adaptation. Use parameters such as selective constraints and priorities to make planning activities more flexible and robust. Agent knowledge description language uses syntax similar to C + +, using predefined classes and functions to realize the description of planning knowledge, to facilitate the process of computing, easy to extend. The descriptive ability of the description language is verified through the example described by the planning model. Model language processing has been applied to the simulation system, you can simulate the application scenarios.
其他文献
针对重复使用运载器(RLV)的自动着陆段(A&L)提出了一种快速的轨迹生成算法。相比于传统航天飞机的策略,该方法并不依赖事先离线计算并储存好的若干轨迹,可在A&L段初始状态存
Background The transcription factor,repressor of GATA-3 (ROG),can simultaneously suppress the expression of T helper cells (Th1 and Th2) cytokines.Since the sup
针对机械飞轮内干扰可能导致小卫星姿态控制系统性能下降问题,提出了一种加入机械飞轮干扰补偿的自适应滑模变结构姿态控制方法。本文针对基于机械飞轮的三轴稳定卫星姿态控
根据三通道偏振导航传感器模型的测量原理,对模型中影响测量精度的偏振正交误差进行了分析和研究,推导出了三通道间偏振光轴的正交误差、定位初始角与定位角测量误差间的关系
针对先进气动布局飞行器飞行包线大、非线性不确定性强、耦合严重等问题给飞行控制带来的挑战,提出了一种基于扩张状态观测器(ESO)的轨迹线性化控制方法,给出了控制器的结构
Background Gastric cancer is one of the most common types of malignant tumors in China and East Asia and has the highest mortality rate of the malignant gastroi
Background Mutations in fumarylacetoacetate hydrolase (FAH) gene can lead to tyrosinemia type 1 (HT1),a relatively rare autosomal recessive disorder.To date,no