Development of flight test platform for flapping wings micro air vehicles
This report presents the design, fabrication process, analysis and characterization of simple and low cost test platforms for force measurement of Flapping Wing Micro Air Vehicles (FWMAVs). Simple pendulum method and linearly guided load cell based test platforms currently used by the research group...
Saved in:
Main Author: | Pradipta, Johanes Eldwin |
---|---|
Other Authors: | Lau Gih Keong |
Format: | Final Year Project |
Language: | English |
Published: |
2015
|
Subjects: | |
Online Access: | http://hdl.handle.net/10356/64582 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Nanyang Technological University |
Language: | English |
Similar Items
-
Development of elastomeric flight muscles for flapping wing micro air vehicles
by: Lau, Gih-Keong, et al.
Published: (2019) -
Development of control system for flapping wing micro air vehicles
by: Chua, Jasper Ming Song
Published: (2017) -
Four-winged flapping compliant mechanisms for micro air vehicles
by: Lee, Chong Han.
Published: (2012) -
Monolithic compliant mechanism for flapping-wing micro air vehicle
by: Ricky Jonathan Tulolo.
Published: (2013) -
Motor simulation G-simulation seat with flaps
by: Li, Qi
Published: (2023)