Use mainly Tal Shima's technical papers for the literature review. My assignment is to reproduce the simulations that are carried out in the technical paper attached. However, the simulations are done considering it's a dual controlled missile (considering nose and tail control effort). Besides, the 2 loop case autopilot design is studied for 3 different set of gains in order to investigate the limiting cases (using only tail control or nose control). The Pareto front is obtained for a perfect interception (each point of the curve should represent a simulation result in terms of nose and tail control) and also a miss ditance Pareto front surface where the nose control effort penalty and the miss distance penalty are changed. Finally, the bandwidth of the control system and the guidance system is obtained and it is analysed how the difference between them varies for the separated, single-loop and 2-loop designs.

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