Abstract
Fleet of flying robots are expected to be applied to various practical tasks such as surveillance, inspection of infrastructures, and rescue. In this study, we aim at realizing precise formation flight of multiple flying robots. To realize precise formation flight, high tracking performance for given path is required. Therefore, tracking controller should be designed. In this paper, tracking control system based on Differential Flatness is designed for small unmanned helicopter. The numerical simulation is carried out to verify the effectiveness of designed tracking controller.
Original language | English |
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Title of host publication | 2015 54th Annual Conference of the Society of Instrument and Control Engineers of Japan, SICE 2015 |
Publisher | Institute of Electrical and Electronics Engineers Inc. |
Pages | 816-819 |
Number of pages | 4 |
ISBN (Electronic) | 9784907764487 |
DOIs | |
Publication status | Published - 2015 Sep 30 |
Externally published | Yes |
Event | 54th Annual Conference of the Society of Instrument and Control Engineers of Japan, SICE 2015 - Hangzhou, China Duration: 2015 Jul 28 → 2015 Jul 30 |
Other
Other | 54th Annual Conference of the Society of Instrument and Control Engineers of Japan, SICE 2015 |
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Country | China |
City | Hangzhou |
Period | 15/7/28 → 15/7/30 |
Keywords
- Differential flatness
- Flying robot
- Formation flight
- Tracking controller
ASJC Scopus subject areas
- Control and Systems Engineering