I need Deliverables part and MATLAB Code for the same.
Description: You will design a target interception system for a missile. The target will move
at a straight line and using the thrust vector controlling the missile should be able to intercept
the target automatically.
1. A mathematical model of the interception system in 2-dimension
2. A control system design
3. Demonstration using Simulink and corresponding 2-dimensional animation
Note that, the thrust is generated due to the gas exhausted through the engine nozzle. The rate
of change of the mass of the missile due to the exhaust gas can be expressed as:
ṁ =T / ISPg where, Isp is sprecific impulse and g = 9.8m/s2