DocumentCode
3572773
Title
Time matching strategy for missiles attack based upon pseudo spectral optimization prediction method
Author
Limin Zhang ; Mingwei Sun ; Zengqiang Chen
Author_Institution
Tianjin Key Lab. of Intell. Robot., Nankai Univ., Tianjin, China
fYear
2014
Firstpage
1670
Lastpage
1675
Abstract
In the process of salvo attack of cruise missile, in order to solve the time matching problem occurring in the flight process, predicting online real-time trajectory optimization based on the pseudo spectral method under the condition of no-fly zones constraint, and the combination circular maneuver are presented. The whole route area of cruise missile is divided, and the method of forward search of no-fly zone to adjust the route online rapidly is provided. Simulation results show that the proposed method can make the cruise missile effectively consume the redundant time and bypass the no-fly zone successfully, the adjust distance is short, and can fly back to the original trajectory in the end of the adjustment, eventually achieve the goal of salvo attack.
Keywords
missiles; trajectory optimisation (aerospace); combination circular maneuver; cruise missile; flight process; missiles attack; no-fly zones constraint condition; online real-time trajectory optimization prediction; pseudospectral optimization prediction method; salvo attack process; time matching strategy; Educational institutions; Intelligent control; Missiles; Optimization; Process control; Real-time systems; Trajectory; circular maneuver; no-fly zone; predicting online real-time trajectory optimization; pseudo spectral; salvo attack;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Control and Automation (WCICA), 2014 11th World Congress on
Type
conf
DOI
10.1109/WCICA.2014.7052971
Filename
7052971
Link To Document