Scientific implications of the Huygens parachute system

1993 ◽  
Author(s):  
RALPH LORENZ
Keyword(s):  
2011 ◽  
Author(s):  
Joseph J. Knapik ◽  
Ryan Steelman ◽  
Kyle Hoedebecke ◽  
Bria Graham ◽  
Shawn Rankin ◽  
...  

1980 ◽  
Vol 17 (8) ◽  
pp. 545-546 ◽  
Author(s):  
P.R. Schatzle ◽  
W.H. Curry

2017 ◽  
Vol 88 (6) ◽  
pp. 556-564 ◽  
Author(s):  
Mustafa Alaziz ◽  
Adrienne Stolfi ◽  
Dean M. Olson

1999 ◽  
Author(s):  
Yoshifumi Inatani ◽  
Takashi Nakajima ◽  
Masahisa Honda ◽  
Motoki Hinada ◽  
Koju Hiraki ◽  
...  
Keyword(s):  

2016 ◽  
Vol 29 (4) ◽  
pp. 06016001 ◽  
Author(s):  
Xiao-Peng Xue ◽  
Yusuke Nishiyama ◽  
Yoshiaki Nakamura ◽  
Koichi Mori ◽  
Chih-Yung Wen

2013 ◽  
Vol 380-384 ◽  
pp. 837-840
Author(s):  
Jin Song ◽  
Jun Ma ◽  
Min Jiang

Parachute system is a significant composing part of aircraft, and the swing angle is one of system security targets. To the complicated measurement problem of parachute angle in wind tunnel test, this paper describes a test method based on stereo vision system, the system is mainly composed of two CCD cameras, image acquisition card and computer. It can get 3D coordinates by stereo vision calibration and digital image processing technology, and calculate the parachute swing angle by geometry relationship. The result shows that the method succeeds, and gets the vertical and horizontal angles which are projected onto two orthogonal planes. The method has the advantage of simple system composing and good compatibility, displays much better application value.


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