Ying Zhang, Dongqiang Shi, Di Peng, Tiantian Li, Qian Zhao
{"title":"指数平滑火箭模式切换算法仿真","authors":"Ying Zhang, Dongqiang Shi, Di Peng, Tiantian Li, Qian Zhao","doi":"10.1109/prmvia58252.2023.00042","DOIUrl":null,"url":null,"abstract":"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.","PeriodicalId":221346,"journal":{"name":"2023 International Conference on Pattern Recognition, Machine Vision and Intelligent Algorithms (PRMVIA)","volume":null,"pages":null},"PeriodicalIF":0.0000,"publicationDate":"2023-03-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Exponentially Smooth Rocket Mode Switching Algorithm Simulation\",\"authors\":\"Ying Zhang, Dongqiang Shi, Di Peng, Tiantian Li, Qian Zhao\",\"doi\":\"10.1109/prmvia58252.2023.00042\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"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.\",\"PeriodicalId\":221346,\"journal\":{\"name\":\"2023 International Conference on Pattern Recognition, Machine Vision and Intelligent Algorithms (PRMVIA)\",\"volume\":null,\"pages\":null},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2023-03-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2023 International Conference on Pattern Recognition, Machine Vision and Intelligent Algorithms (PRMVIA)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/prmvia58252.2023.00042\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2023 International Conference on Pattern Recognition, Machine Vision and Intelligent Algorithms (PRMVIA)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/prmvia58252.2023.00042","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
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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