DocumentCode
3404720
Title
Angular Glint of Aircraft Formation and Its Applications
Author
Shi, Xiaoli ; Liu, Yongcai ; Wang, Xinmin ; Wang, Changqing
Author_Institution
Northwestern Polytech. Univ., Xian
fYear
2007
fDate
5-8 Aug. 2007
Firstpage
1334
Lastpage
1339
Abstract
The problem of angular glint of flying vehicle formation and its application in anti-interception is studied. The angular glint of the flying vehicle formation is modeled as evenly distributed N-point scattering centers with method of phase gradient, and the linear errors of the angular glint and its distribution characteristics are calculated. Finally, simulations of conflicts of a formation consists of four aircraft against a typical surface-to-air missile were done, the results of which verified the effectiveness of the method proposed.
Keywords
aircraft control; position control; aircraft formation; angular glint; antiinterception; distributed N-point scattering centers; flying vehicle formation; phase gradient; surface-to-air missile; Aerospace engineering; Airborne radar; Aircraft propulsion; Automation; Frequency; Mechatronics; Missiles; Radar scattering; Radar tracking; Vehicles; aircraft formation; angular glint; anti-interception; extended target; phase gradient;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronics and Automation, 2007. ICMA 2007. International Conference on
Conference_Location
Harbin
Print_ISBN
978-1-4244-0828-3
Electronic_ISBN
978-1-4244-0828-3
Type
conf
DOI
10.1109/ICMA.2007.4303743
Filename
4303743
Link To Document