A Flight Dynamics Helicopter UAV Model For A Single Pitch-Lag-Flap Main Rotor: Model Extensions
A Flight Dynamics Helicopter UAV Model For A Single Pitch-Lag-Flap Main Rotor: Model Extensions
| dc.contributor.author | Taamallah, S. | en_US |
| dc.date.accessioned | 2013-11-11T09:11:54Z | |
| dc.date.available | 2013-11-11T09:11:54Z | |
| dc.date.issued | 2010 | en_US |
| dc.identifier.other | NLR-TP-2010-286-PT-2 | en_US |
| dc.identifier.uri | http://hdl.handle.net/10921/910 | |
| dc.language.iso | en | en_US |
| dc.publisher | National Aerospace Laboratory NLR | en_US |
| dc.relation.ispartofseries | NLR Technical Publication;2010-286-PT-2 | en_US |
| dc.subject.other | Unmanned aircraft systems (UAS) | en_US |
| dc.subject.other | Helicopters | en_US |
| dc.title | A Flight Dynamics Helicopter UAV Model For A Single Pitch-Lag-Flap Main Rotor: Model Extensions | en_US |
Files
Original bundle
1 - 1 of 1
- Name:
- TP-2010-286-2.pdf
- Size:
- 373.43 KB
- Format:
- Adobe Portable Document Format
- Description: