{"title":"利用陀螺力矩器的有理分式方法和自旋卫星姿态控制","authors":"P. K. De, A. Iyer","doi":"10.1109/ACC.1989.4173456","DOIUrl":null,"url":null,"abstract":"The problem of joint stabilization and tracking of a spinning satellite system in addition to its regulation are considered. Rational Fractional approach is used to obtain coprime equations in a multivariate setting. Parameterized compensators are obtained for regulation and, simultaneous stabilization and tracking cases. Simulation results are presented to show the accomplishment of attitude control in different settings with simple control inputs.","PeriodicalId":383719,"journal":{"name":"1989 American Control Conference","volume":"54 5 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1989-06-21","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"4","resultStr":"{\"title\":\"Rational Fraction Approach and Attitude Control of Spinning Satellite using Gyrotorquer\",\"authors\":\"P. K. De, A. Iyer\",\"doi\":\"10.1109/ACC.1989.4173456\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The problem of joint stabilization and tracking of a spinning satellite system in addition to its regulation are considered. Rational Fractional approach is used to obtain coprime equations in a multivariate setting. Parameterized compensators are obtained for regulation and, simultaneous stabilization and tracking cases. Simulation results are presented to show the accomplishment of attitude control in different settings with simple control inputs.\",\"PeriodicalId\":383719,\"journal\":{\"name\":\"1989 American Control Conference\",\"volume\":\"54 5 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1989-06-21\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"4\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"1989 American Control Conference\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ACC.1989.4173456\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"1989 American Control Conference","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ACC.1989.4173456","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Rational Fraction Approach and Attitude Control of Spinning Satellite using Gyrotorquer
The problem of joint stabilization and tracking of a spinning satellite system in addition to its regulation are considered. Rational Fractional approach is used to obtain coprime equations in a multivariate setting. Parameterized compensators are obtained for regulation and, simultaneous stabilization and tracking cases. Simulation results are presented to show the accomplishment of attitude control in different settings with simple control inputs.
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