DocumentCode
2813896
Title
Influencing factor and corresponding method of target drone dynamic stability
Author
Xiao, Jun ; Zhang, Weiwei ; Han, Yujie ; Sun, Min
fYear
2011
fDate
15-17 July 2011
Firstpage
4998
Lastpage
5001
Abstract
The longitudinal motion equations were built by mathematical model of target drone movement. The longitudinal linearized equation was got by the linearization of longitudinal motion equations. The modality character was analysed by the solution. According to remolding motion, the effection on dynamic stability by flight speed, height and centroid position variation was researched and corresponding methods were obtained. That advanced the ability of target drone support and training flight security.
Keywords
aircraft; stability; centroid position; flight security; flight speed; influencing factor; longitudinal linearized equation; longitudinal motion equations; mathematical model; modality character; remolding motion; target drone dynamic stability; target drone movement; Aerospace control; Aerospace electronics; Atmospheric modeling; Dynamics; Equations; Mathematical model; Stability analysis; dynamic stability; modality; target drone;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechanic Automation and Control Engineering (MACE), 2011 Second International Conference on
Conference_Location
Hohhot
Print_ISBN
978-1-4244-9436-1
Type
conf
DOI
10.1109/MACE.2011.5988138
Filename
5988138
Link To Document