Please use this identifier to cite or link to this item:
https://doi.org/10.1016/j.mechatronics.2013.07.004
DC Field | Value | |
---|---|---|
dc.title | A bumpless hybrid supervisory control algorithm for the formation of unmanned helicopters | |
dc.contributor.author | Karimoddini, A. | |
dc.contributor.author | Lin, H. | |
dc.contributor.author | Chen, B.M. | |
dc.contributor.author | Lee, T.H. | |
dc.date.accessioned | 2014-04-24T07:18:52Z | |
dc.date.available | 2014-04-24T07:18:52Z | |
dc.date.issued | 2013-09 | |
dc.identifier.citation | Karimoddini, A., Lin, H., Chen, B.M., Lee, T.H. (2013-09). A bumpless hybrid supervisory control algorithm for the formation of unmanned helicopters. Mechatronics 23 (6) : 677-688. ScholarBank@NUS Repository. https://doi.org/10.1016/j.mechatronics.2013.07.004 | |
dc.identifier.issn | 09574158 | |
dc.identifier.uri | http://scholarbank.nus.edu.sg/handle/10635/50837 | |
dc.description.abstract | This paper presents a bumpless hybrid supervisory control scheme for the formation of unmanned helicopters. The approach is based on the polar partitioning of the space, from which a finite bisimilar quotient transition system of the original continuous variable control system is obtained. Then, to implement the designed hybrid supervisory control algorithm, a hierarchical control structure is introduced with a discrete supervisor on the top layer that is connected to the regulation layer via an interface layer. Transiting over the partitioned space may cause jumps on the generated control signal which is harmful for a real flight system. Hence, a smooth control mechanism is introduced that has no jump when the system's trajectory transits from one region to its adjacent region while preserving the bisimulation relation between the abstract model and the original partitioned system. Several actual flight tests have been conducted to verify the algorithm and the control performance. © 2013 Elsevier Ltd. All rights reserved. | |
dc.description.uri | http://libproxy1.nus.edu.sg/login?url=http://dx.doi.org/10.1016/j.mechatronics.2013.07.004 | |
dc.source | Scopus | |
dc.subject | Formation control | |
dc.subject | Hybrid supervisory control | |
dc.subject | Implementation issues | |
dc.subject | Unmanned aerial vehicles (UAVs) | |
dc.type | Article | |
dc.contributor.department | ELECTRICAL & COMPUTER ENGINEERING | |
dc.description.doi | 10.1016/j.mechatronics.2013.07.004 | |
dc.description.sourcetitle | Mechatronics | |
dc.description.volume | 23 | |
dc.description.issue | 6 | |
dc.description.page | 677-688 | |
dc.description.coden | MECHE | |
dc.identifier.isiut | 000324719800014 | |
Appears in Collections: | Staff Publications |
Show simple item record
Files in This Item:
There are no files associated with this item.
SCOPUSTM
Citations
7
checked on Mar 24, 2023
WEB OF SCIENCETM
Citations
7
checked on Mar 24, 2023
Page view(s)
250
checked on Mar 16, 2023
Google ScholarTM
Check
Altmetric
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.