A Simple Differential Sliding Mode Design for the Overload Control of Missile System |
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| Journal | Applied Mechanics and Materials (Volumes 66 - 68) |
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| Volume | Mechanical, Materials and Manufacturing Engineering |
| Edited by | Honghua Tan |
| Pages | 207-211 |
| DOI | 10.4028/www.scientific.net/AMM.66-68.207 |
| Citation | Wen Guang Zhang et al., 2011, Applied Mechanics and Materials, 66-68, 207 |
| Online since | July, 2011 |
| Authors | Wen Guang Zhang, Jun Wei Lei, Jie Cheng |
| Keywords | Differential, Overload, Sliding Mode, Stability |
| Abstract | A simple differential sliding mode control law was designed for the missile overload control system without considering the uncertainties of air-dynamic coefficients. The sliding mode was composed of overload error and the differential error of overload. Finally, a numerical simulation was down and it testified that it is unable to make the system stable with only pure overload control strategy. Although the sliding mode was arrived , Oscillation phenomenon was caused by the poles in imaginary axis. |
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