DocumentCode :
233389
Title :
Air conflict resolution algorithm based on optimal control
Author :
Lu Yanjun ; Zhang Bo ; Zhang Xiaodong
Author_Institution :
Sch. of Autom., Shenyang Aerosp. Univ., Shenyang, China
fYear :
2014
fDate :
28-30 July 2014
Firstpage :
8919
Lastpage :
8923
Abstract :
In order to address the issue of conflict resolution between aircrafts, an improved algorithm based on optimal control theory is presented by which collision avoidance with other aircraft could be achieved with a minimum change on the original route. At first, an optimal escape maneuver is formulated to be a variable terminal-time optimal control problem with a compound performance index. Secondly the model of conflict resolution is set up, which is combined with the dynamics model of an aircraft. Finally, according to minimum principle, the optimal control problem is solved and consequently an optimal route is obtained. Simulation results show that for a collision danger in air with different flight heading or altitude, the algorithm could give an optimal route for conflict resolution.
Keywords :
aircraft control; collision avoidance; minimum principle; time optimal control; vehicle dynamics; air conflict resolution algorithm; aircraft dynamics model; collision avoidance; compound performance index; minimum principle; optimal escape maneuver; variable terminal-time optimal control problem; Aerospace control; Aircraft; Atmospheric modeling; Collision avoidance; Equations; Mathematical model; Optimal control; Conflict Resolution; Optimal Control; Optimal Route;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (CCC), 2014 33rd Chinese
Conference_Location :
Nanjing
Type :
conf
DOI :
10.1109/ChiCC.2014.6896501
Filename :
6896501
Link To Document :
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