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Veronte Autopilot design for a fixed wing aircraft using Matlab and Simulink

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1. PI controller architecture  of Veronte Autopilot to be developed in Simulink for a fixed wing UAV. Reference will be provided.
2. Gain tuning to be done for different flight stages-climb, take-off, cruise, hold, loitre, weave, Pop-up, pop-down, low-level and towing and the values Kp, Ki, Ti (integral time parameter), Td (derivative time parameter) and Tau (Discrete filter paramter) must be tabulated for those flight stages.
In towing, the aerial target will have a sleeve (a ballistic body) attached to it by a string during take-off, which will be released in air after attaining steady state flight. Reference to be provided.
3. 3D plot representation of flight envelope.