scholarly journals Low-speed optic-flow sensor onboard an unmanned helicopter flying outside over fields

Author(s):  
Guillaume Sabiron ◽  
Paul Chavent ◽  
Thibaut Raharijaona ◽  
Patrick Fabiani ◽  
Franck Ruffier
2007 ◽  
Vol 133 (1) ◽  
pp. 88-95 ◽  
Author(s):  
Marko Pudas ◽  
Stéphane Viollet ◽  
Franck Ruffier ◽  
Arvi Kruusing ◽  
Stéphane Amic ◽  
...  

2004 ◽  
Author(s):  
Wei Peng ◽  
Gary R. Pickrell ◽  
Juncheng Xu ◽  
Zhengyu Huang ◽  
Dae Woong Kim ◽  
...  

2016 ◽  
Vol 12 (6) ◽  
pp. 20160221 ◽  
Author(s):  
Ingo Schiffner ◽  
Mandyam V. Srinivasan

How do flying birds respond to changing environments? The behaviour of budgerigars, Melopsittacus undulatus , was filmed as they flew through a tapered tunnel. Unlike flying insects—which vary their speed progressively and continuously by holding constant the optic flow induced by the walls—the birds showed a tendency to fly at only two distinct, fixed speeds. They switched between a high speed in the wider section of the tunnel, and a low speed in the narrower section. The transition between the two speeds was abrupt, and anticipatory. The high speed was close to the energy-efficient, outdoor cruising speed for these birds, while the low speed was approximately half this value. This is the first observation of the existence of two distinct, preferred flight speeds in birds. A dual-speed flight strategy may be beneficial for birds that fly in varying environments, with the high speed set at an energy-efficient value for flight through open spaces, and the low speed suited to safe manoeuvring in a cluttered environment. The constancy of flight speed within each regime enables the distances of obstacles and landmarks to be directly calibrated in terms of optic flow, thus facilitating simple and efficient guidance of flight through changing environments.


1996 ◽  
Author(s):  
Aidong Meng ◽  
Shanglian Huang ◽  
Weimin Chen ◽  
Fei Luo

2013 ◽  
Vol 380-384 ◽  
pp. 459-462
Author(s):  
Yu Hu Du ◽  
Jian Cheng Fang

Compared with the fixed-wing aerial vehicles, small-scale unmanned helicopter (SUH) has the advantages of taking off and landing vertically, cruising under ultra low speed, and sustained hovering in the air. SUH has properties of nonlinear, unstable, strongly coupling, and applying control system for SUH is considered as a challenging task. This paper presents the design of the flight control system for a SUH. This flight control system consists of two parts, namely, ground station and onboard part. Various experiments have been conducted to test the performance of this flight control system, and some of the results are presented at the end.


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