Name
Abstract | ||
|---|---|---|
Presents a cluster controller design of a mesh of helicopters which produces the trajectory to be tracked in terms of the desired acceleration. As an intermediate step for the formation flying of a cluster of helicopters, an individual helicopter controller is designed which accepts the trajectory to be tracked in terms of the desired accelerations. The design uses the fact that the linear position dynamics of a helicopter are slow compared to the attitude dynamics. Next, we discuss the design of a higher-level cluster controller assuming simple double-integrator dynamics. The results show that we need leader information to achieve mesh stability in case of point masses. The higher-level mesh controller is then used for the simulation of a formation flight of a cluster of helicopters. It is observed that the intuition about mesh stability obtained with simple double-integrator dynamics is carried over to the case of helicopters |
Year | DOI | Venue |
|---|---|---|
2001 | 10.1109/ACC.2001.945514 | American Control Conference, 2001. Proceedings of the 2001 |
Keywords | DocType | Volume |
acceleration,aircraft control,control system synthesis,helicopters,mobile robots,multi-robot systems,stability,tracking,acceleration,attitude dynamics,cluster controller design,double integrator dynamics,formation flying,helicopters,leader information,linear position dynamics,mesh stability,point masses,simulation,trajectory tracking,unmanned aerial vehicle clusters | Conference | 1 |
ISSN | ISBN | Citations |
0743-1619 | 0-7803-6495-3 | 12 |
PageRank | References | Authors |
5.64 | 0 | 4 |
Name | Order | Citations | PageRank |
|---|---|---|---|
| Pant, A. | 1 | 12 | 5.64 |
| Seiler, P. | 2 | 26 | 11.39 |
| Koo, T.J. | 3 | 12 | 5.64 |
| Hedrick, K. | 4 | 12 | 5.64 |