Optimal Control and Flight Trajectory Optimization Applied to EvasionAnalysis英文电子书.pdf

Optimal Control and Flight Trajectory Optimization Applied to EvasionAnalysis英文电子书.pdf

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OPTIMAL CONTROL AND FLIGHT TRAJECTORY OPTIMIZATION APPLIED TO EVASION ANALYSIS Licentiate Thesis Jukka Ranta March 2004 Systems Analysis Laboratory Department of Engineering Physics and Mathematics Helsinki University of Technology FI-02150 Espoo HELSINKI UNIVERSITY ABSTRACT OF OF TECHNOLOGY LICENTIATE’S THESIS Department of Engineering Physics and Mathematics Author: Jukka Ranta Department: Department of Engineering Physics and Mathematics Major subject: Systems and Operations Research Minor subject: Systems Engineering English title: Optimal control and flight trajectory optimization ap- plied to evasion analysis Finnish title: Optimis¨a¨at¨o ja lentoratojen optimointi sovellettuna v¨aist¨oanalyysiin Number of pages: 102 Chair: Mat-2 Applied Mathematics Supervisor: Professor Raimo P. H¨am¨al¨ainen Instructor: Dr.Tech. Tuomas Raivio Abstract: This thesis deals with the numerical solution of optimal control problems arising from aircraft trajectory optimization and evasion analysis. The Introduction con- siders optimal control problems, solution methods for them, dynamic modeling of flight vehicles, and flight trajectory optimization in general. Encounter scenarios between an aircraft and a missile are considered. The missile pursues the aircraft, which in turn tries to avoid being hit. The methodology is based on dynamic modeling of the vehicles and optimal control theory. The missi

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