Name
Abstract | ||
|---|---|---|
In this paper, an augmentation strategy is designed for the steady-state error caused by the coupling between ballistic and attitude. It can process and transform a class of nonlinear systems. Based on this, a slip form controller is designed. In the design process of the controller, a sliding surface that can be damped is calculated, and precise control of the system is realized. Then it is applied to the attitude control of the reentry vehicle, which effectively solves the problem of attitude angle control accuracy caused by the coupling between the ballistic and the attitude. |
Year | DOI | Venue |
|---|---|---|
2019 | 10.1109/ICCA.2019.8899551 | 2019 IEEE 15TH INTERNATIONAL CONFERENCE ON CONTROL AND AUTOMATION (ICCA) |
Field | DocType | ISSN |
Control theory,Coupling,Nonlinear system,Control theory,Slip (materials science),Attitude control,Control engineering,Engineering design process,Engineering | Conference | 1948-3449 |
Citations | PageRank | References |
0 | 0.34 | 0 |
Authors | ||
6 | ||
Name | Order | Citations | PageRank |
|---|---|---|---|
| Rong Ma | 1 | 0 | 0.68 |
| Peicheng Liu | 2 | 0 | 0.68 |
| Xianqiang Li | 3 | 0 | 1.01 |
| Yihong Quan | 4 | 0 | 0.34 |
| Di Pan | 5 | 0 | 0.68 |
| Yanze Zhu | 6 | 0 | 0.34 |