| contributor author | Der-Cherng Liaw | |
| contributor author | Yew-Wen Liang | |
| contributor author | Chiz-Chung Cheng | |
| date accessioned | 2017-05-09T00:01:57Z | |
| date available | 2017-05-09T00:01:57Z | |
| date copyright | December, 2000 | |
| date issued | 2000 | |
| identifier issn | 0022-0434 | |
| identifier other | JDSMAA-26273#663_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/123421 | |
| description abstract | Variable Structure Control (VSC) technique is applied to the design of robust homing missile guidance laws. In the design procedure, the target’s maneuver is assumed to be unpredictable and is considered as disturbances. Guidance laws are then proposed to achieve the interception performance for both cases of longitude-axis control being available and unavailable. The proposed guidance laws are continuous which alleviate chattering drawback by classic VSC design. Results are obtained and compared with those by realistic true proportional navigation design to illustrate the benefits of the proposed design. [S0022-0434(00)00604-3] | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Nonlinear Control for Missile Terminal Guidance | |
| type | Journal Paper | |
| journal volume | 122 | |
| journal issue | 4 | |
| journal title | Journal of Dynamic Systems, Measurement, and Control | |
| identifier doi | 10.1115/1.1316796 | |
| journal fristpage | 663 | |
| journal lastpage | 668 | |
| identifier eissn | 1528-9028 | |
| keywords | Design | |
| keywords | Missiles | |
| keywords | Navigation AND Motion | |
| tree | Journal of Dynamic Systems, Measurement, and Control:;2000:;volume( 122 ):;issue: 004 | |
| contenttype | Fulltext | |
