Development of Centimeter‐sized Aerial Vehicles

From the viewpoints of stability and safety in outdoor flights, a centimeter-sized UAV probably has a larger possibility to be used in our everyday lives than different sized UAVs. Centimeter-sized fixed-wing UAVs that have already been developed can make autonomous flights. However, their flight speed, that is, their momentum, is fairly high. To use them, their flight speed must be decreased. On the other hand, centimeter-sized rotary-wing UAVs that have also already been developed can also make autonomous flights. However, their weight is fairly large. To use them in our daily life, their weight must be decreased. Longer flight duration is also required. For both fixed-wing and rotary-wing UAVs, higher reliability is also required. Keywords: centimeter-sized vehicle; MAV; fixed-wing; rotary-wing; flight controller; low Reynolds number; wing characteristics; stability

[1]  M H Dickinson,et al.  Leading-Edge Vortices Elevate Lift of Autorotating Plant Seeds , 2009, Science.

[2]  Shigeru Sunada,et al.  Comparison of wing characteristics at an ultralow Reynolds number , 2002 .

[3]  Takashi Abe,et al.  Design guidelines of rotary wings in hover for insect-scale micro air vehicle applications , 2007 .

[4]  Hiroshi Tokutake,et al.  Stability analysis of gliding flight of a swallowtail butterfly Papilio xuthus. , 2009, Journal of theoretical biology.

[5]  J. Gordon Leishman,et al.  Understanding the Aerodynamic Efficiency of a Hovering Micro-Rotor , 2008 .

[6]  Jin Fujinaga,et al.  Guidance and Control of a Small Unmanned Aerial Vehicle and Autonomous Flight Experiments , 2008 .

[7]  Eric N. Johnson,et al.  Modeling, Control, and Flight Testing of a Small Ducted-Fan Aircraft , 2005 .

[8]  Michael Athans,et al.  Gain and phase margin for multiloop LQG regulators , 1976, 1976 IEEE Conference on Decision and Control including the 15th Symposium on Adaptive Processes.

[9]  Darryll J. Pines,et al.  Design, Analysis and Hover Performance of a Rotary Wing Micro Air Vehicle , 2003 .

[10]  E. Laitone Wind tunnel tests of wings at Reynolds numbers below 70 000 , 1997 .

[11]  D. Pines,et al.  Challenges Facing Future Micro-Air-Vehicle Development , 2006 .

[12]  Shigeru Sunada,et al.  Effects of Reynolds Number on Characteristics of Fixed and Rotary Wings , 2004 .

[13]  Inderjit Chopra,et al.  Hover Tests of Micro Aerial Vehicle-Scale Shrouded Rotors, Part I: Performance Characteristics , 2009 .