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mat_MissileGuidanceSim

V2018.4.4: Created.

V2018.4.7: PN finished.

V2018.4.8.1152: Time step set to 0.001s fixed. Visualization outputs dynamically.

V2018.4.8.1816: Add PPN & APN choosing module. Update visualization.

V2018.4.8.2034: Signs of acceleration modified.

V2018.4.9.1530: Three blocks (PPN, TPN, APN) are put together. Trajectory and overload comparing figures can be output.

V2018.4.9.2051: OGL added. But the overload seems wrong. The K_Guide_OGL gets huge as tgo approaches 0.

V2018.4.10.0956: OGL modified.

Need to do: LOS rate (Omega) = LOS - LOS_old;

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2D Simulation of missile guidance system.

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