{"title":"太空中最佳火箭机动","authors":"M. Pachter, G. Chatterji, M. Tahk","doi":"10.1109/ACC.1989.4173543","DOIUrl":null,"url":null,"abstract":"The problem is addressed of optimally steering a vehicle in space, controlled by thrust vectoring, to affect a demanded change in heading and achieve maximal terminal speed. The optimal solution is explicitly derived and it is presented in a readily implementable form.","PeriodicalId":383719,"journal":{"name":"1989 American Control Conference","volume":"176 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1989-06-21","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Optimal Rocket Maneuvers in Space\",\"authors\":\"M. Pachter, G. Chatterji, M. Tahk\",\"doi\":\"10.1109/ACC.1989.4173543\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The problem is addressed of optimally steering a vehicle in space, controlled by thrust vectoring, to affect a demanded change in heading and achieve maximal terminal speed. The optimal solution is explicitly derived and it is presented in a readily implementable form.\",\"PeriodicalId\":383719,\"journal\":{\"name\":\"1989 American Control Conference\",\"volume\":\"176 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1989-06-21\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"1989 American Control Conference\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ACC.1989.4173543\",\"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.1989.4173543","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
The problem is addressed of optimally steering a vehicle in space, controlled by thrust vectoring, to affect a demanded change in heading and achieve maximal terminal speed. The optimal solution is explicitly derived and it is presented in a readily implementable form.
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