Szerző dc.contributor.author | Papp István | |
Szerző dc.contributor.author | Szilvássy László | |
Szerző dc.contributor.author | Óvári Gyula | |
Elérhetőség dátuma dc.date.accessioned | 2019-12-04T08:19:18Z | |
Rendelkezésre állás dátuma dc.date.available | 2019-12-04T08:19:18Z | |
Kiadás dc.date.issued | 2015 | |
Issn dc.identifier.issn | 2498-5392 | |
Uri dc.identifier.uri | http://hdl.handle.net/20.500.12944/14428 | |
Kivonat dc.description.abstract | In order to guide itself to a successful target intercept, the missile must obtain inormation about the target. The prelaunch and post launch information too, must be gathered. Before a missile is launched, that is, during the prelaunch phase, the missile needs to know where to go. It knows that it is supposed to go to the target, but it must be told where the target is. The missile is told where the target is by electrical signals entering through the umbilical from the launcher. These signals are head aimed (to point the missile head at the target), English bias (to point the missile at the intercept point), and an estimate of true target Doppler on the simulated Doppler line. | hu_HU |
Nyelv dc.language.iso | en | hu_HU |
Kulcsszó dc.subject | missile | hu_HU |
Kulcsszó dc.subject | equations of motion | hu_HU |
Kulcsszó dc.subject | guidance | hu_HU |
Kulcsszó dc.subject | derivation | hu_HU |
Cím dc.title | Derivation of the Fundamental Missile Guidance Equations | hu_HU |
Típus dc.type | Folyóiratcikk | hu_HU |
Változat dc.description.version | kiadói | hu_HU |
Doi azonosító dc.identifier.doi | 10.32565/aarms.2015.4.8 | |
Folyóirat dc.identifier.journalTitle | AARMS | hu_HU |
Évfolyam dc.identifier.journalVolume | 14 | hu_HU |
dc.identifier.page | 341-348 | hu_HU |
Füzetszám dc.identifier.journalIssueNumber | 4 | hu_HU |