المؤلفون: Karelahti, Janne

المساهمون: Department of Engineering Physics and Mathematics, Teknillisen fysiikan ja matematiikan osasto, Systems Analysis Laboratory, Systeemianalyysin laboratorio, Aalto-yliopisto, Aalto University

مصطلحات موضوعية: Physics, Mathematics, air combat, missile avoidance, computational optimal control, game theory, receding horizon control, adaptive control, Bayesian reasoning, influence diagram, inverse simulation, ilmataistelu, ohjuksenväistö, laskennallinen optimisäätö, peliteoria, etenevän suunnitteluhorisontin säätö, adaptiivinen säätö, Bayes-päättely, vaikutuskaavio, käänteissimulointi

وصف الملف: 30, [75]; application/pdf

Relation: Research reports / Helsinki University of Technology, Systems Analysis Laboratory. A; 99; Karelahti, J., Virtanen, K., and Raivio, T., Near-Optimal Missile Avoidance Trajectories via Receding Horizon Control, Journal of Guidance, Control, and Dynamics, Vol. 30, No. 5, 2007, pp. 1287-1298. [article1.pdf] © 2007 American Institute of Aeronautics and Astronautics (AIAA). By permission.; Karelahti, J. and Virtanen, K., Adaptive Controller for the Avoidance of an Unknownly Guided Air Combat Missile, Proceedings of the 46th IEEE Conference on Decision and Control, 2007. [article2.pdf] © 2007 IEEE. By permission.; Karelahti, J., Virtanen, K., and Öström, J., Automated Generation of Realistic Near-Optimal Aircraft Trajectories, Journal of Guidance, Control, and Dynamics, accepted for publication. [article3.pdf] © 2008 by authors and © 2008 American Institute of Aeronautics and Astronautics (AIAA). By permission.; Virtanen, K., Karelahti, J., and Raivio, T., Modeling Air Combat by a Moving Horizon Influence Diagram Game, Journal of Guidance, Control, and Dynamics, Vol. 29, No. 5, 2006, pp. 1080-1091. [article4.pdf] © 2006 American Institute of Aeronautics and Astronautics (AIAA). By permission.; Karelahti, J., Virtanen, K., and Raivio, T., Game Optimal Support Time of a Medium Range Air-to-Air Missile, Journal of Guidance, Control, and Dynamics, Vol. 29, No. 5, 2006, pp. 1061-1069. [article5.pdf] © 2006 American Institute of Aeronautics and Astronautics (AIAA). By permission.; https://aaltodoc.aalto.fi/handle/123456789/2983; urn:nbn:fi:tkk-011119

الاتاحة: https://aaltodoc.aalto.fi/handle/123456789/2983