nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
1 |
A CFD Study on Leading Edge Wing Surface Modification of a Low Aspect Ratio Flying Wing to Improve Lift Performance
|
Ramprasadh, C. |
|
2015 |
|
3 |
p. 361-373 |
artikel |
2 |
A miniature seven-hole probe air data system and its application on spin prediction
|
Li, Shaoze |
|
2016 |
|
3 |
p. 143-154 |
artikel |
3 |
An Evaluation of Multi-Rotor Unmanned Aircraft as Flying Wind Sensors
|
Marino, Matthew |
|
2015 |
|
3 |
p. 285-299 |
artikel |
4 |
A Numerical Model to Study the Nonlinear and Unsteady Aerodynamics of Bioinspired Morphing-Wing Concepts
|
Verstraete, Marcos L. |
|
2015 |
|
3 |
p. 327-345 |
artikel |
5 |
Application of a lattice Boltzmann method to some challenges related to micro-air vehicles
|
Gourdain, Nicolas |
|
2018 |
|
3 |
p. 285-299 |
artikel |
6 |
A Review of Biomimetic Air Vehicle Research: 1984-2014
|
Ward, Thomas A. |
|
2015 |
|
3 |
p. 375-394 |
artikel |
7 |
A Structural Dynamic Analysis of a Manduca Sexta Forewing
|
Sims, Travis W. |
|
2010 |
|
3 |
p. 119-140 |
artikel |
8 |
Bioinspired wind field estimation—part 1: Angle of attack measurements through surface pressure distribution
|
Gavrilovic, Nikola |
|
2018 |
|
3 |
p. 273-284 |
artikel |
9 |
Control of a hybrid helicopter with wings
|
De Wagter, Christophe |
|
2017 |
|
3 |
p. 209-217 |
artikel |
10 |
Design, development, and flight testing of a high endurance micro quadrotor helicopter
|
Winslow, Justin |
|
2016 |
|
3 |
p. 155-169 |
artikel |
11 |
Design Optimisation of a Reconfigurable Perching Element for Vertical Take-Off and Landing Unmanned Aerial Vehicles
|
Erbil, Mehmet Ali |
|
2013 |
|
3 |
p. 207-228 |
artikel |
12 |
Design, Performance and Testing of a Quad Rotor Biplane Micro Air Vehicle for Multi Role Missions
|
Hrishikeshavan, Vikram |
|
2014 |
|
3 |
p. 155-173 |
artikel |
13 |
Development and Testing of a Quad Rotor Smartphone Control System for Novice Users
|
Cummings, M.L. |
|
2012 |
|
3 |
p. 165-178 |
artikel |
14 |
Development of a meso-scale cycloidal-rotor aircraft for micro air vehicle application
|
Shrestha, Elena |
|
2017 |
|
3 |
p. 218-231 |
artikel |
15 |
Development of Experimental Facilities for Multi-Mission MAVs
|
Thipyopas, Chinnapat |
|
2010 |
|
3 |
p. 141-156 |
artikel |
16 |
Distance and velocity estimation using optical flow from a monocular camera
|
Ho, Hann Woei |
|
2017 |
|
3 |
p. 198-208 |
artikel |
17 |
Dynamic Simulation of an Unmanned Hybrid Flying Robot
|
Alsaif, khalid A. |
|
2015 |
|
3 |
p. 257-273 |
artikel |
18 |
Editorial IJMAV
|
Moschetta, Jean-Marc |
|
2018 |
|
3 |
p. 243 |
artikel |
19 |
Effect of wing flexibility on flight dynamics stability of flapping wing MAVs in forward flight
|
Xue, Dong |
|
2016 |
|
3 |
p. 170-180 |
artikel |
20 |
Energy-Harvesting Mechanisms for UAV Flight by Dynamic Soaring
|
Bonnin, V. |
|
2015 |
|
3 |
p. 213-229 |
artikel |
21 |
Evaluation of Nano-Scale Rotors and Motors at Static Condition
|
Liu, Zhen |
|
2013 |
|
3 |
p. 193-206 |
artikel |
22 |
Evaluation of the Thorax of Manduca Sexta for Flapping Wing Micro Air Vehicle Applications
|
Cranston, Brian |
|
2014 |
|
3 |
p. 191-210 |
artikel |
23 |
Experimental Investigation of Micro Air Vehicle Scale Helicopter Rotor in Hover
|
Benedict, Moble |
|
2015 |
|
3 |
p. 231-255 |
artikel |
24 |
Experimental investigation of wing flexibility on force generation of a hovering flapping wing micro air vehicle with double wing clap-and-fling effects
|
Nguyen, Quoc V |
|
2017 |
|
3 |
p. 187-197 |
artikel |
25 |
Experimental investigation on flow characteristics of a four-wing micro air vehicle
|
Shi, Lisong |
|
2016 |
|
3 |
p. 181-193 |
artikel |
26 |
Experimental Study of Reynolds Number and Gust Influence on Transient Force and Flow Generated by a Robotic Hummingbird
|
Tian, Ruijun |
|
2015 |
|
3 |
p. 347-360 |
artikel |
27 |
Exploring tandem wing UAS designs for operation in turbulent urban environments
|
Gigacz, Rohan |
|
2018 |
|
3 |
p. 254-261 |
artikel |
28 |
Flapping Flight Stability in Hover: A Comparison of Various Aerodynamic Models
|
Karásek, Matěj |
|
2012 |
|
3 |
p. 203-226 |
artikel |
29 |
Force Measurements and Flow Visualization for a Flexible Flapping Wing Mechanism
|
Massey, Kevin |
|
2009 |
|
3 |
p. 183-202 |
artikel |
30 |
Force Measurements on Locusts during Visually-Evoked Collision Avoidance Maneuvers
|
Kumar, Rajeev |
|
2012 |
|
3 |
p. 227-249 |
artikel |
31 |
Ground/Wall Effects on a Tilting Ducted Fan
|
Hosseini, Zahra |
|
2011 |
|
3 |
p. 119-141 |
artikel |
32 |
High-Amplitude Pitch of a Flat Plate: An Abstraction of Perching and Flapping
|
Ol, Michael V. |
|
2009 |
|
3 |
p. 203-216 |
artikel |
33 |
High Performance Propeller System for a Multi-Mission Micro Aerial Vehicle
|
Thipyopas, Chinnapat |
|
2013 |
|
3 |
p. 179-191 |
artikel |
34 |
Influence of Turbulence on MAV Roll Perturbations
|
Mohamed, A. |
|
2014 |
|
3 |
p. 175-190 |
artikel |
35 |
Numerical and experimental investigation of an airfoil design for a Martian micro rotorcraft
|
Désert, T |
|
2018 |
|
3 |
p. 262-272 |
artikel |
36 |
Numerical and Experimental Simulations of Flapping Wings
|
Yuan, Weixing |
|
2010 |
|
3 |
p. 181-209 |
artikel |
37 |
On the Unsteady Behavior of the Flow around NACA 0012 Airfoil with Steady External Conditions at Re=1000
|
Kurtulus, Dilek Funda |
|
2015 |
|
3 |
p. 301-326 |
artikel |
38 |
Optimal Guidance of a Relay Aircraft to Extend Small Unmanned Aircraft Range
|
Pachter, Meir |
|
2010 |
|
3 |
p. 157-180 |
artikel |
39 |
Optimal Settings of Aerodynamic Performance Parameters in Hovering Flight
|
Dong, Haibo |
|
2009 |
|
3 |
p. 173-181 |
artikel |
40 |
Parametric Representation and Shape Optimization of Flapping Micro Air Vehicle Wings
|
Stewart, Eric C. |
|
2012 |
|
3 |
p. 179-202 |
artikel |
41 |
Passive Roll Compensation on Micro Air Vehicles with Perimeter Reinforced Membrane Wings
|
Cantrell, Jason T. |
|
2013 |
|
3 |
p. 163-177 |
artikel |
42 |
Passive Rotation Joint Design Considerations for Lift and Thrust Generation for a Biomimetic Flapping Wing
|
Lindholm, Garrison J. |
|
2014 |
|
3 |
p. 141-154 |
artikel |
43 |
Performance Flight Testing of Small, Electric Powered Unmanned Aerial Vehicles
|
Ostler, Jon N. |
|
2009 |
|
3 |
p. 155-171 |
artikel |
44 |
Quad-thopter: Tailless flapping wing robot with four pairs of wings
|
De Wagter, Christophe |
|
2018 |
|
3 |
p. 244-253 |
artikel |
45 |
The Complicating Effect of Uncertain Flapping Wing Kinematics on Model Validation
|
Stanford, Bret |
|
2011 |
|
3 |
p. 143-148 |
artikel |
46 |
The Energy Benefits of the Pantograph Wing Mechanism in Flapping Flight: Case Study of a Gull
|
Burgess, S.C. |
|
2015 |
|
3 |
p. 275-283 |
artikel |
47 |
The Evaluation of a Biologically Inspired Engineered MAV Wing Compared to the Manduca Sexta Wing under Simulated Flapping Conditions
|
DeLeón, Nathanial E. |
|
2011 |
|
3 |
p. 149-168 |
artikel |
48 |
Ultra-wideband based cooperative relative localization algorithm and experiments for multiple unmanned aerial vehicles in GPS denied environments
|
Guo, Kexin |
|
2017 |
|
3 |
p. 169-186 |
artikel |
49 |
Visual Tracking in Wind with Field of View Constraints
|
Saunders, Jeffery |
|
2011 |
|
3 |
p. 169-182 |
artikel |
50 |
Vortex structure on twist-morphing micro air vehicle wings
|
Ismail, NI |
|
2016 |
|
3 |
p. 194-205 |
artikel |