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