Name
Abstract | ||
|---|---|---|
Based on previous work, a Nussbaum gian controller is proposed to solve the unknown input direction problem of a large family of supersonic missiles. Also considering the one order dynamic characteristic of actuator, the uncertainties of nonlinear missile system, which is assumed to satisfy the so-called bounded uncertainty condition, are coped by the adopting of integral action and backstepping technology. And the unknown control direction problem of supersonic missile is solved by adopting of the Nussbaum gain method. A novel analysis with Lyapunov function and Nussbaum gain function are completed and the stability of the whole system is guaranteed by constructing of the Lyapunov function. |
Year | DOI | Venue |
|---|---|---|
2011 | 10.1007/978-3-642-23321-0_97 | ADVANCES IN COMPUTER SCIENCE, ENVIRONMENT, ECOINFORMATICS, AND EDUCATION, PT I |
Keywords | Field | DocType |
Adaptive,Nussbaum Gain,Missile,Control | Lyapunov function,Control theory,Backstepping,Nonlinear system,Missile,Control theory,Supersonic speed,Adaptive control,Mathematics,Bounded function | Conference |
Volume | ISSN | Citations |
214 | 1865-0929 | 0 |
PageRank | References | Authors |
0.34 | 1 | 4 |
Name | Order | Citations | PageRank |
|---|---|---|---|
| Jinhua Wu | 1 | 4 | 1.60 |
| Junwei Lei | 2 | 30 | 11.27 |
| Wenjin Gu | 3 | 13 | 5.63 |
| Jianhong Shi | 4 | 8 | 3.38 |