Dawoon Jung, J. Kwon, Kwang-yul Baek, Han Woong Ahn, Jong-Wook Choi
{"title":"韩国探路者月球轨道器姿态控制模拟器的动态三维可视化","authors":"Dawoon Jung, J. Kwon, Kwang-yul Baek, Han Woong Ahn, Jong-Wook Choi","doi":"10.23919/ICCAS50221.2020.9268408","DOIUrl":null,"url":null,"abstract":"Visualizing the Korea Pathfinder Lunar Orbiter (KPLO) attitude control behavior is useful for verifying dynamical characteristics unseen in previous Earth-orbiting satellite missions. This paper describes a visualization component of the LUNASIM simulator running unmodified attitude control flight software that is able to communicate with an external program to animate realistically in three dimensions the simulated attitude and orbital state, thruster firings, and solar array rotations of KPLO at faster-than real-time speeds for intuitive design verification. Visualization is also supported when LUNASIM is connected to a processor emulator in a fully end-to-end simulated ETB environment. Results are presented illustrating accurate spacecraft dynamics during special mission scenarios such as roll maneuvering while Sun-pointing near the ecliptic plane, yaw-flipped lunar orbit attitude, and slewing to image the lunar surface while in 45-degree tilted attitude. These results demonstrate the value of visualizing attitude control simulator output for novel spacecraft missions.","PeriodicalId":6732,"journal":{"name":"2020 20th International Conference on Control, Automation and Systems (ICCAS)","volume":"8 1","pages":"788-792"},"PeriodicalIF":0.0000,"publicationDate":"2020-10-13","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Dynamic 3-D Visualization of the Korea Pathfinder Lunar Orbiter Attitude Control Simulator\",\"authors\":\"Dawoon Jung, J. Kwon, Kwang-yul Baek, Han Woong Ahn, Jong-Wook Choi\",\"doi\":\"10.23919/ICCAS50221.2020.9268408\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Visualizing the Korea Pathfinder Lunar Orbiter (KPLO) attitude control behavior is useful for verifying dynamical characteristics unseen in previous Earth-orbiting satellite missions. This paper describes a visualization component of the LUNASIM simulator running unmodified attitude control flight software that is able to communicate with an external program to animate realistically in three dimensions the simulated attitude and orbital state, thruster firings, and solar array rotations of KPLO at faster-than real-time speeds for intuitive design verification. Visualization is also supported when LUNASIM is connected to a processor emulator in a fully end-to-end simulated ETB environment. Results are presented illustrating accurate spacecraft dynamics during special mission scenarios such as roll maneuvering while Sun-pointing near the ecliptic plane, yaw-flipped lunar orbit attitude, and slewing to image the lunar surface while in 45-degree tilted attitude. These results demonstrate the value of visualizing attitude control simulator output for novel spacecraft missions.\",\"PeriodicalId\":6732,\"journal\":{\"name\":\"2020 20th International Conference on Control, Automation and Systems (ICCAS)\",\"volume\":\"8 1\",\"pages\":\"788-792\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2020-10-13\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2020 20th International Conference on Control, Automation and Systems (ICCAS)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.23919/ICCAS50221.2020.9268408\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2020 20th International Conference on Control, Automation and Systems (ICCAS)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.23919/ICCAS50221.2020.9268408","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Dynamic 3-D Visualization of the Korea Pathfinder Lunar Orbiter Attitude Control Simulator
Visualizing the Korea Pathfinder Lunar Orbiter (KPLO) attitude control behavior is useful for verifying dynamical characteristics unseen in previous Earth-orbiting satellite missions. This paper describes a visualization component of the LUNASIM simulator running unmodified attitude control flight software that is able to communicate with an external program to animate realistically in three dimensions the simulated attitude and orbital state, thruster firings, and solar array rotations of KPLO at faster-than real-time speeds for intuitive design verification. Visualization is also supported when LUNASIM is connected to a processor emulator in a fully end-to-end simulated ETB environment. Results are presented illustrating accurate spacecraft dynamics during special mission scenarios such as roll maneuvering while Sun-pointing near the ecliptic plane, yaw-flipped lunar orbit attitude, and slewing to image the lunar surface while in 45-degree tilted attitude. These results demonstrate the value of visualizing attitude control simulator output for novel spacecraft missions.