/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

Primary LanguageMATLABMIT LicenseMIT

Missile-Guidance-and-RL

  • 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