指数平滑火箭模式切换算法仿真

2023 International Conference on Pattern Recognition, Machine Vision and Intelligent Algorithms (PRMVIA) Pub Date : 2023-03-01 DOI:10.1109/prmvia58252.2023.00042

Ying Zhang, Dongqiang Shi, Di Peng, Tiantian Li, Qian Zhao

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引用次数: 0

摘要

火箭在交付后具有多种工作模式，根据其独特的飞行器特性，本文提出了一种指数平滑火箭模式切换算法。模式切换造成的固定延迟也可能影响正常工作模式的启动时间，所以只有在空闲时间较短时才进入浅睡眠模式。当长时间空闲时，系统需要切换到深度睡眠模式，以最大限度地降低系统功耗。对模式切换的延时和功耗进行了分析和验证。通过数学建模，选取最小的MRE重量参数，满足火箭多工作模式间可靠、快速切换的要求。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Exponentially Smooth Rocket Mode Switching Algorithm Simulation

The rocket has a variety of working modes after delivery, and according to its unique aircraft characteristics, this paper proposes an exponentially smooth rocket mode switching algorithm. The fixed delay caused by mode switching may also affect the startup time of normal working mode, so only enter shallow sleep mode when the idle time is short. When idle for a long time, the system needs to switch to deep sleep mode, where the power consumption of the system is minimized. The delay and power consumption of mode switching are analyzed and verified. After mathematical modeling, the smallest weight parameter of MRE is taken to meet the requirements of reliable and fast switching between multiple working modes of the rocket.

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来源期刊

2023 International Conference on Pattern Recognition, Machine Vision and Intelligent Algorithms (PRMVIA)

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