Effects of Time-Varying Inertias on Flight Dynamics of an Asymmetric Variable-Sweep Morphing Aircraft-Reference-Cited by-同舟云学术

Effects of Time-Varying Inertias on Flight Dynamics of an Asymmetric Variable-Sweep Morphing Aircraft

Published:2007-06-15 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference and Exhibit
language:
Short-container-title:

Author:

Grant Daniel¹,Lind Rick¹

Affiliation:

1. University of Florida

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-6487

Reference38 articles.

1. Area (cm2) -15 -30 66.17 14.68 1028.11 -10 -20 73.97 13.12 1003.45 -5 -10 78.81 12.38 976.25 0 0 80.39 11.84 947.11 5 10 78.61 11.62 916.68 10 20 73.61 11.69 885.66 15 30 65.72 12.13 854.76

2. element X Y Z Ixx Iyy Izz Ixy Ixz Iyz battery -2.5 0.0 -1.75 398 1211 812.5 0.0 -596 0.0 fuselage 0.0 0.0 -1.75 903 903 0.0 0.0 0.0 0.0

3. motor 4.5 0.0 1.5 113 1125 1013 0.0 -338 0.0 tail boom 8.5 0.0 -3.0 135 1219 1084 0.0 383 0.0

4. vertical tail 13.5 0.0 0.0 0.0 1458 1458 0.0 0.0 0.0 horizontal tail 13.5 0.0 -3.0 72 1530 1458 0.0 324 0.0 Table 3. Characteristics of Elements given as Centroid Position (in) and Moments of Inertia (g ·in2)

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