Name
Abstract | ||
|---|---|---|
The quadrotor aircraft has the characteristics of nonlinearity, strong coupling and underactivity, which is a useful tool for researchers to test and evaluate new ideas in many different fields, including flight control theory, real time systems, and robot navigation. In order to reduce the non-essential disturbance factors and accident rate during the flight, and we independently design a test platform to test quadrotor flight attitude. Through the force analysis and dynamic modeling of the system, the attitude controller is designed by back-stepping control algorithm which can stabilize quickly. The stability of flight attitude is verified on Matlab environment and the platform respectively. The experimental results show that the platform design is reasonable and feasible, and it is an effective test platform. |
Year | DOI | Venue |
|---|---|---|
2018 | 10.1109/ICARCV.2018.8581388 | 2018 15TH INTERNATIONAL CONFERENCE ON CONTROL, AUTOMATION, ROBOTICS AND VISION (ICARCV) |
Field | DocType | ISSN |
Back stepping,Control theory,Nonlinear system,Coupling,MATLAB,Force analysis,Computer science,Control engineering,System dynamics,Robot | Conference | 2474-2953 |
Citations | PageRank | References |
0 | 0.34 | 0 |
Authors | ||
4 | ||
Name | Order | Citations | PageRank |
|---|---|---|---|
| Kai Cao | 1 | 2 | 3.43 |
| Jiajia Gao | 2 | 0 | 0.34 |
| Song Gao | 3 | 24 | 5.20 |
| Chaobo Chen | 4 | 0 | 1.35 |