| 面向平行系统的飞行器航迹仿真模型架构设计 |
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| 作者姓名： | 王凯旋 李烨 薛晨琛 董宇 |
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| 作者单位： | 中国运载火箭技术研究院，北京 100076 |
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| 基金项目： | 军科委重点基础研究项目 |
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| 摘 要： | 面向平行系统运行需求，对飞行器航迹计算的积分、抽象计算、数学模型等进行建模和架构设计，实现了航迹计算过程中数据与算法的分离，并采用继承和指针注册机制完成与航迹计算相关的数据统一化分层管理，通过对飞行器状态转移模型的设计实现了飞行器不同状态或阶段之间航迹的顺利衔接，能够实现多状态并行转移和执行，以抵消平行系统不确定性和随机性的影响，为平行系统运行提供灵活、高效的仿真模型。
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| 关 键 词： | 平行系统 飞行器航迹计算 架构设计 |
A Flight Track Simulation Model Architecture for
Parallel Simulation System |
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| Authors: | WANG Kaixuan LI Ye XUE Chenchen DONG Yu |
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| Institution: | China Academy of Launch Vehicle Technology,Beijing 100076, China |
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| Abstract: | Rotating detonation engine (RDE) is one of the new types of aerospace engines based on detonation combustion. In recent years, due to advantages of one-initiation, high thermal efficiency and compact size, RDE has attracted wide attention from the propulsion community. In this paper, recent progress in RDE has been reviewed from the aspects of flow-field structures, operating modes, stability, and propulsion performance. Key problems of RDE are summarized finally. |
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| Keywords: | Parallel system Aircraft track calculation Architecture design |
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