Szerző dc.contributor.author | Papp István | |
Elérhetőség dátuma dc.date.accessioned | 2019-12-10T09:09:28Z | |
Rendelkezésre állás dátuma dc.date.available | 2019-12-10T09:09:28Z | |
Kiadás dc.date.issued | 2017 | |
Issn dc.identifier.issn | 2498-5392 | |
Uri dc.identifier.uri | http://hdl.handle.net/20.500.12944/14605 | |
Kivonat dc.description.abstract | Recently, aerospace (flight) engineers, having more solid mathematical backgrounds, have become familiar with the newest results in control theory and are able not only to formulate control problems but also solve them without attracting the attention of control experts. Moreover, they try to apply new results in control theory to specific aerospace and missile guidance problems. As a result, control theory is losing its biggest supplier and, to a certain degree, this slows down its progress. | hu_HU |
Nyelv dc.language.iso | en | hu_HU |
Kulcsszó dc.subject | mathematical | hu_HU |
Kulcsszó dc.subject | control | hu_HU |
Kulcsszó dc.subject | missile | hu_HU |
Kulcsszó dc.subject | equations of motion | hu_HU |
Cím dc.title | Missile Mathematical Model and System Design | hu_HU |
Típus dc.type | Folyóiratcikk | hu_HU |
Változat dc.description.version | kiadói | hu_HU |
Doi azonosító dc.identifier.doi | 10.32565/aarms.2017.1.3 | |
Folyóirat dc.identifier.journalTitle | AARMS | hu_HU |
Évfolyam dc.identifier.journalVolume | 16 | hu_HU |
dc.identifier.page | 29-35 | hu_HU |
Füzetszám dc.identifier.journalIssueNumber | 1 | hu_HU |