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Backstepping Controller Design for a Kind of High Speed Vehicle
| Content Provider | Semantic Scholar |
|---|---|
| Author | Zhang, Wenguang Lin, Zijian Lei, Junwei |
| Copyright Year | 2016 |
| Abstract | A kind of backstepping controller is designed for a kind of pitch channel model of hypersonic aircrafts. The main task is to realize attack angle tracking of hypersonic aircrafts. Compared with traditional linear design method, the main difference is that the nonlinear model is directly used in the design process by adopting a Lyapunov function method to guarantee the stability of the whole system. At last, detailed simulations are done to show the rightness of the proposed method. |
| File Format | PDF HTM / HTML |
| DOI | 10.2991/icmmbe-16.2016.43 |
| Alternate Webpage(s) | https://download.atlantis-press.com/article/25860759.pdf |
| Alternate Webpage(s) | https://doi.org/10.2991/icmmbe-16.2016.43 |
| Language | English |
| Access Restriction | Open |
| Content Type | Text |
| Resource Type | Article |
