| contributor author | Zhou, Di | |
| contributor author | Sun, Sheng | |
| contributor author | Zhou, Jing Yang | |
| contributor author | Teo, Kok Lay | |
| date accessioned | 2017-05-09T01:16:15Z | |
| date available | 2017-05-09T01:16:15Z | |
| date issued | 2015 | |
| identifier issn | 0022-0434 | |
| identifier other | ds_137_02_024501.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/157459 | |
| description abstract | Based on the discrete form of the targetmissile relative motion equations in plane, a discrete slidingmode guidance (DSMG) law is proposed. All previous missile seeker's measurements are used in the design of the DSMG law to estimate the target acceleration such that noises in the seeker's measurements are effectively being smoothened. It is proved that the proposed DSMG law is finite time convergent. Quasi slidingmode bands of the DSMG law are discussed, and the formula for calculating the terminal miss distances of the missile under the DSMG law are presented. Simulation results from a space interception process verify the effectiveness of the proposed method. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | A Discrete Sliding Mode Guidance Law | |
| type | Journal Paper | |
| journal volume | 137 | |
| journal issue | 2 | |
| journal title | Journal of Dynamic Systems, Measurement, and Control | |
| identifier doi | 10.1115/1.4028038 | |
| journal fristpage | 24501 | |
| journal lastpage | 24501 | |
| identifier eissn | 1528-9028 | |
| tree | Journal of Dynamic Systems, Measurement, and Control:;2015:;volume( 137 ):;issue: 002 | |
| contenttype | Fulltext | |