Name
Abstract | ||
|---|---|---|
The overload control of missile system is researched under the condition that the control direction is unknown. A nussbaum gain strategy is adopted to solve the unknown control direction problem for the linear model of missile motion of pitch channel. The backstepping technology and integral action are used to cope the system uncertainty. A novel type of control law, which is only consisted of overload signal and angle velocity of missile, is constructed and the stability of whole system is guaranteed by a whole Lyapunov function. The defect of the proposed method is that the dyanmic of control fin is not considered. |
Year | DOI | Venue |
|---|---|---|
2011 | 10.1007/978-3-642-23321-0_96 | ADVANCES IN COMPUTER SCIENCE, ENVIRONMENT, ECOINFORMATICS, AND EDUCATION, PT I |
Keywords | Field | DocType |
Backstepping,Uncertainty,Nussbaum Gain,Supersonic Missile,Overload Control | Lyapunov function,Fin,Backstepping,Missile,Linear model,Computer science,Control theory,Communication channel,Overload control,Automatic gain control | Conference |
Volume | Issue | ISSN |
214 | PART 1 | 1865-0929 |
Citations | PageRank | References |
0 | 0.34 | 1 |
Authors | ||
4 | ||
Name | Order | Citations | PageRank |
|---|---|---|---|
| Jianhong Shi | 1 | 8 | 3.38 |
| Guorong Zhao | 2 | 8 | 2.58 |
| Junwei Lei | 3 | 30 | 11.27 |
| Guoqiang Liang | 4 | 6 | 2.87 |