- Studied RL agent based Guidance Laws and Optimal Control techniques for Surface-to-Air Missile Guidance
- Simulated optimal trajectory for surface to air ballistic missile by implementing Gradient method as optimization technique in MATLAB under the guidance of Dr. Prem Kumar(Scientist- ‘F’, DOS)}
- Implemented Proportional Navigation(PN Classical Guidance law) on a point mass 3-d model in MATLAB with lofting and used it as a baseline for performance evaluation against RL agent based guidance laws
sankalp-s/Missile-Guidance-and-RL
Studied RL agent-based Guidance Laws and Optimal Control techniques for Surface-to-Air Missile Guidance. Simulated optimal trajectory for the surface to air ballistic missile by implementing Gradient method as optimization technique in MATLAB
MATLABMIT