DocumentCode
3026450
Title
Recent advances in optimal pursuit and evasion
Author
Shinar, J. ; Gutman, S.
Author_Institution
Technion, Israel Institute of Technology, Haifa, Israel
fYear
1979
fDate
10-12 Jan. 1979
Firstpage
960
Lastpage
965
Abstract
The missile-aircraft pursuit-evasion problem is formulated by a three-dimensional linearized kinematic model. The formulation is valid both for the optimal control (against a known adversary strategy) and the zero sum differential game versions. Assuming perfect information the linearized kinematic model yields for both versions a solution which can be implemented in real-time for airborne application. The avoidance of a known pursuer by an evader who has no state information is solved by a stochastically optimal periodical maneuver. Other examples of imperfect information are briefly discussed.
Keywords
Acceleration; Aerodynamics; Kinematics; Missiles; Optimal control; Vehicle dynamics;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control including the 17th Symposium on Adaptive Processes, 1978 IEEE Conference on
Conference_Location
San Diego, CA, USA
Type
conf
DOI
10.1109/CDC.1978.268074
Filename
4046261
Link To Document