Analysis and Design of Control Systems for Aircraft and Missiles
| dc.citation.epage | 28 | en_US |
| dc.citation.issue | 2 | en_US |
| dc.citation.spage | 12 | en_US |
| dc.citation.volume | 1 | en_US |
| dc.contributor.author | 韓光渭 | zh_TW |
| dc.contributor.author | K. W. Han | en_US |
| dc.date.accessioned | 2017-10-06T06:17:37Z | |
| dc.date.available | 2017-10-06T06:17:37Z | |
| dc.date.issued | 1966-04 | en_US |
| dc.description.abstract | In this paper, control systems for aircraft and missiles are analyzed and designed using a "stability curve" method which is particularily suitable for testing stability and adjusting parameters for complex control systems. Design procedures are given along with examples. | en_US |
| dc.identifier.journal | 交大學刊 | zh_TW |
| dc.identifier.journal | science bulletin national chiao-tung university | en_US |
| dc.identifier.uri | https://ir.lib.nycu.edu.tw/handle/11536/137437 | |
| dc.language.iso | en_US | en_US |
| dc.publisher | 交大學刊編輯委員會 | zh_TW |
| dc.title | Analysis and Design of Control Systems for Aircraft and Missiles | en_US |
| dc.type | Campus Publications | en_US |