Micro Aerial Vehicle, Flapping Wing, Genetic Algorithm, Optimization, Force Measurement, Flow Visualization, Hovering Flight.
The development of Micro Aerial Vehicles (MAV) is driven by its potential use as a vehicle that can perform remote observation in hazardous environment. Because of the operational Reynolds number of MAV is low, flapping wing type MAV is supposed to be superior to other types. Currently, there are no...
Saved in:
Main Author: | Satria Palar, Pramudita |
---|---|
Format: | Theses |
Language: | Indonesia |
Subjects: | |
Online Access: | https://digilib.itb.ac.id/gdl/view/38896 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Institut Teknologi Bandung |
Language: | Indonesia |
Similar Items
-
PRELIMINARY WING MECHANISM DESIGN AND CFD ANALYSIS OF FLAPPING WING MINI UNMANNED AERIAL VEHICLE
by: Duke Tantono, Albert -
COMPUTATIONAL AERODYNAMICS AND FLIGHT SIMULATION BASED FLIGHT TEST PLAN DESIGN FOR UNMANNED AERIAL VEHICLE
by: Akhdiyatullah G., Syahrahman -
PARAMETRIC STUDY ON TACTICAL UNMANNED AERIAL VEHICLES (TUAV) WINGS BASED ON AEROELASTIC PERFORMANCE
by: Gede Anjastara Bandem, I -
MULTIMODE FLIGHT CONTROL SYSTEM OF UNMANNED COMBAT AERIAL VEHICLE (UCAV) USING EIGENSTRUCTURE ASSIGNMENT METHOD
by: Valmay Priyono, Aathirah -
OPTIMISASI KARAKTERISTIK RADAR CROSS SECTION PADA UNMANNED COMBAT AERIAL VEHICLE BERBENTUK FLYING WING MENGGUNAKAN PERANGKAT LUNAK FEKO
by: Perbawamukti Hidayat, Shiddiq