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Online since: November 2012
Authors: Ali Shakoori, Mahdi Mortazavi, Hadi Nobahari
Weight, mass
n3/σ
Moment of inertia
n5/σ
Fig. 1 DSM system internal arrangement
Table 2: Full-scale aircraft weights and moments of inertia
Weight (kgf)
X_cg
Y_cg
Z_cg (m)
Ixx
Iyy
Izz
Ixz (kg.m2)
442.2
3.18
0
0.03
44.8
875.2
896
19.52
Table 3: DSM weights and moments of inertia
Weight (kgf)
X_cg
Y_cg
Z_cg (m)
Ixx
Iyy
Izz
Ixz (kg.m2)
55.28
1.59
0.00
0.015
1.4
27.35
28
0.61
At first, for designed initial possible DSM configuration, based on its components weight (mi) and coordinates (Xcg,Ycg,Zcg); an estimation of CG position and moments is obtained.
Online since: July 2011
Authors: Li Shuang Liu
Vol.29 ( 2008), p892-896 (In Chinese)
[3] Rob O’Reilly, Tang Huy, Chen Wei: IEEE SENSORS 2008 Conference, p148-151
[4] Yunbo Shi, Xiaojin Qi, Jiu Liu: chinese journal of mechanical engineering,Vol.9(2008), p200-203(In Chinese)
[5] Chenghua Wang, Peiyin Chen, Xiaocheng Xu: Explosion and Shock Wave, Vol.27 (2007) (In Chinese)
[6] Jiarong Huang, Ruichao Liu, Xiang He: Explosion and Shock Wave, Vol.5 (2009) (In Chinese)